CN108304596A - A kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat - Google Patents
A kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat Download PDFInfo
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Abstract
A kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat disclosed by the embodiments of the present invention, it is related to aircraft below deck equipment radiation/phenomenon of Heat analytical technology, can solves the problems, such as that the slow precision of temperature data acquisition speed of below deck equipment is low.This method analyses the high temperature heat sources such as battery in cabin and establishes corresponding below deck equipment to the radiant heat transfer amount of below deck equipment and absorb radiant heat flux database first；Consider further that the radiation of high temperature heat source, equipment self-heating, air conduction, Three-dimensional Heat-transfer, analyze the temperature of below deck equipment, ultimate analysis below deck equipment temperature rises mechanism, it is proposed the major measure of control below deck equipment Wen Sheng, foundation, this method is instructed to be mainly used for hypersonic aircraft below deck equipment radiation/phenomenon of Heat analysis to improve thermal environment proposition in cabin.
Description
Technical field
The present invention relates to aircraft below deck equipment radiation/phenomenon of Heat analysis technical fields, more particularly to one kind is for height
The analysis method of supersonic aircraft below deck equipment radiation/phenomenon of Heat.
Background technology
Increasingly longer with the flight time of high-speed aircraft, high-speed aircraft becomes increasingly complex, and below deck equipment is increasingly
More, the working time of below deck equipment and supplying cell also increases.In the case, battery accumulates the radiant heat of each equipment in cabin
The fever accumulation phenomenon of tired, each equipment itself is increasingly severe, it is possible to which below deck equipment temperature is more than safe handling temperature, flight
There are risks for experiment.
The couple solution in thermal environment study emphasis cabin flow field/temperature field in current country outer analysis cabin, using this method
The fine flow field of comparison/thermo parameters method situation can be obtained, but grid and amount of calculation are very big, calculating speed and grid
Configuration, complexity and method of value solving have much relations, cannot meet type of project unit simultaneously to calculating speed and standard
The requirement of true property.
As current high-speed aircraft below deck equipment increases, cable is covered in cabin, remaining space is small, air can not convection current,
The principal element for influencing below deck equipment temperature at this time is the radiant heating of high temperature heat source (such as battery), equipment self-heating, sky
Heat conduction of the gas from high temperature heat source to equipment.For this situation, need to develop a kind of aircraft below deck equipment radiation/phenomenon of Heat
Rapid analysis method quick and precisely assesses below deck equipment temperature.
Invention content
It is an object of the invention to overcome the shortage of prior art, provide a kind of for hypersonic aircraft below deck equipment
The analysis method of radiation/phenomenon of Heat can solve the problems, such as that the slow precision of temperature data acquisition speed of below deck equipment is low.
Technical solution of the invention：
A kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat, this method includes following
Step：
It determines and the high temperature heat source of radiant heating is generated to below deck equipment and obtains the temperature of high temperature heat source；
The grid that high temperature heat source calculates below deck equipment radiant heat transfer amount is generated, which only includes air-grid, normal direction
Size difference between adjacent mesh is less than 1.5~3 times；
Carry out high temperature heat source using the grid to calculate the radiant heat transfer amount of below deck equipment, be analyzed using radiation patterns
The radiant heat flux that below deck equipment absorbs when high temperature heat source irradiates the below deck equipment of different temperatures obtains under below deck equipment different temperatures
The database of radiant heat flux is absorbed, the database includes between below deck equipment node coordinate, wall temperature and absorption radiant heat flux
Correspondence；
The heat transfer grid of below deck equipment is generated, which only includes structural thermal grid, and the size difference between adjacent mesh is small
In 1.5~3 times；
It determines that the self-heating power of below deck equipment, the power are only used for self-heating and elevate the temperature, is not used in equipment
Work；
Carry out below deck equipment Three-dimensional Heat-transfer temperature computation using the structural thermal grid, below deck equipment outer surface it is net
Hot-fluid includes radiant heat flux, below deck equipment self-heating hot-fluid, air conduction hot-fluid, the outside spoke of equipment itself high temperature that it is absorbed
The hot-fluid penetrated.The radiant heat flux that below deck equipment outer surface absorbs, each node when calculating below deck equipment outer surface is every
The respective temperature of a time step all extract real-times, then corresponding hot-fluid is extracted from the absorption radiant heat flux lane database, it will be each
On this node, below deck equipment self-heating hot-fluid is self-heating power divided by table for the radiant heat flux load absorbed at a temperature of
Area, air conduction hot-fluid are obtained using the engineering method of one-dimensional linear heat transfer, hot-fluid of equipment itself high temperature to external radiation
It is obtained using grey-body radiation formula.It is analyzed using heat transfer model and is led in high temperature heat source radiant heating, equipment self-heating, air
Temperature of hot, equipment itself high temperature to below deck equipment under the comprehensive function of external radiation.
A kind of analysis side for hypersonic aircraft below deck equipment radiation/phenomenon of Heat provided in an embodiment of the present invention
Method analyzes the high temperature heat sources such as battery in cabin and establishes corresponding radiant heat flux data to the radiant heat transfer amount of below deck equipment first
Library；Radiation, equipment self-heating and the heat transfer for considering further that high temperature heat source, analyze the temperature of below deck equipment, finally, analyze and are set in cabin
Standby temperature rises mechanism, proposes the major measure of control below deck equipment Wen Sheng, and foundation is instructed to improve thermal environment proposition in cabin.
Description of the drawings
Included attached drawing is used for providing being further understood from the embodiment of the present invention, and which constitute one of specification
Point, for illustrating the embodiment of the present invention, and come together with verbal description to illustrate the principle of the present invention.It should be evident that below
Attached drawing in description is only some embodiments of the present invention, for those of ordinary skill in the art, is not paying creation
Property labour under the premise of, other drawings may also be obtained based on these drawings.
Fig. 1 is the inertial navigation and electric control box temperature in the embodiment of the present invention under different heat exchange approach.
Specific implementation mode
Specific embodiments of the present invention are described in detail below in conjunction with attached drawing.In the following description, for solution
Purpose and not restrictive is released, elaborates detail, to help to be apparent from the present invention.However, to people in the art
It is readily apparent that the present invention can also be put into practice in the other embodiments departing from these details for member.
It should be noted that in order to avoid having obscured the present invention because of unnecessary details, only show in the accompanying drawings
The device structure closely related with scheme according to the present invention and/or processing step are gone out, and have been omitted with relationship of the present invention not
Big other details.
The embodiment of the present invention provides a kind of analysis side for hypersonic aircraft below deck equipment radiation/phenomenon of Heat
Method, this method rises mechanism by analyzing below deck equipment temperature, and then proposes the major measure of control below deck equipment Wen Sheng, for improving
Thermal environment in cabin has good scientific meaning and future in engineering applications.
Specifically, this approach includes the following steps：
It determines and the high temperature heat source of radiant heating is generated to below deck equipment and obtains the temperature of high temperature heat source；
The grid that high temperature heat source calculates below deck equipment radiant heat transfer amount is generated, which only includes air-grid, normal direction
Size difference between adjacent mesh is less than 1.5~3 times；
Carry out high temperature heat source using the grid to calculate the radiant heat transfer amount of below deck equipment, be analyzed using radiation patterns
The radiant heat flux that below deck equipment absorbs when high temperature heat source irradiates the below deck equipment of different temperatures obtains under below deck equipment different temperatures
The database of radiant heat flux is absorbed, the database includes between below deck equipment node coordinate, wall temperature and absorption radiant heat flux
Correspondence；
The heat transfer grid of below deck equipment is generated, which only includes structural thermal grid, and the size difference between adjacent mesh is small
In 1.5~3 times；
It determines that the self-heating power of below deck equipment, the power are only used for self-heating and elevate the temperature, is not used in equipment
Work；
Carry out below deck equipment Three-dimensional Heat-transfer temperature computation using the structural thermal grid, below deck equipment outer surface it is net
Hot-fluid includes radiant heat flux, below deck equipment self-heating hot-fluid, air conduction hot-fluid, the outside spoke of equipment itself high temperature that it is absorbed
The hot-fluid penetrated.The radiant heat flux that below deck equipment outer surface absorbs, each node when calculating below deck equipment outer surface is every
The respective temperature of a time step all extract real-times, then corresponding hot-fluid is extracted from the absorption radiant heat flux lane database, it will be each
On this node, below deck equipment self-heating hot-fluid is self-heating power divided by table for the radiant heat flux load absorbed at a temperature of
Area, air conduction hot-fluid are obtained using the engineering method of one-dimensional linear heat transfer, hot-fluid of equipment itself high temperature to external radiation
It is obtained using grey-body radiation formula.It is analyzed using heat transfer model and is led in high temperature heat source radiant heating, equipment self-heating, air
Temperature of hot, equipment itself high temperature to below deck equipment under the comprehensive function of external radiation.
A kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat provided in this embodiment,
First, the high temperature heat sources such as battery in cabin are analyzed, corresponding radiant heat flux database is established to the radiant heat transfer amount of below deck equipment；Again
Radiation, equipment self-heating and the heat transfer for considering high temperature heat source, analyze the temperature of below deck equipment, finally, analyze below deck equipment temperature
Mechanism is risen, proposes the major measure of control below deck equipment Wen Sheng, foundation is instructed to improve indoor environment proposition.
Understand for the ease of reader, the above method is illustrated below by specific example：
Step 1：It analyzes the high temperature heat sources such as battery in cabin and corresponding radiant heat is established to the radiant heat transfer amount of below deck equipment
Flow database；
Step 1.1 analysis generates the high temperature heat source of radiant heating to below deck equipment and determines the temperature of high temperature heat source, usually
The high temperature heat source that radiant heating is generated to below deck equipment is mainly battery, and the temperature of battery shock wave back casing is 350 DEG C.
Step 1.2 generates the grid that high temperature heat source calculates below deck equipment radiant heat transfer amount
The grid does not include the structured grid of high temperature heat source and below deck equipment, only includes the air-shed grid in cabin, is used for
The ascent of analyzing radiation heat output, it is of less demanding to mesh quality, require nothing more than that grid transition is good, orthogonality is good.
Step 1.3 is carried out high temperature heat source and is calculated the radiant heat transfer amount of below deck equipment
There are two types of analysis methods：
(1) Fluent softwares are utilized, radiation heat-transfer model is opened, set temperature, the transmitting of high temperature heat source and below deck equipment
Rate data, the net radiation hot-fluid (Radiation of below deck equipment when calculating the below deck equipment of high temperature heat source irradiation different temperatures
Heat Flux), establish the database of below deck equipment wall surface (temperature, net radiation hot-fluid).
Temperature after battery shock wave is 350 DEG C, and below deck equipment temperature raising after by electromagnetic radiation judges that only electromagnetic radiation draws
It plays device temperature and does not exceed 350 DEG C.Emissivity, the temperature data of battery and below deck equipment are set, carried out in cell irradiation cabin
Device analysis obtains the net radiation hot-fluid (Radiation Heat Flux) of below deck equipment, establish below deck equipment wall surface (temperature,
Net radiation hot-fluid) database when, selected equipment wall surface temperature is respectively 280K, 290K, 300K, 310K ... 650K.Due to
Radiation equation and energy equation are restrained quickly, and the calculating time of each example only has more than ten seconds, radiation net radiation heat flow data library
Total time-consuming is less than 1 hour.
(2) Fluent softwares are utilized, radiation heat-transfer model is opened, set temperature, the transmitting of high temperature heat source and below deck equipment
Rate data, radiant heat flux (the Absorbed Radiation that below deck equipment absorbs when calculating high temperature heat source irradiation below deck equipment
Flux)。
Since the rapid analysis method that this patent proposes does not need fine flow field, and the very difficult convergence of flow equation,
It calculates and takes very much, in order to improve computational efficiency, flow equation need not be solved, only solve radiation patterns equation and heat transfer side
Journey.
Step 2：Radiation, equipment self-heating and the heat transfer for considering high temperature heat source, analyze the temperature of below deck equipment.
Step 2.1 generates the heat transfer grid of below deck equipment
For analyzing below deck equipment heat transfer, it is desirable that grid transition is good, orthogonality is good.
Step 2.2 determines the self-heating power of below deck equipment
The power is the power that below deck equipment is only used for self-heating, is not the operating power of equipment.Below deck equipment inertial navigation
Heating power with electric control box is 20W.
Step 2.3 calculates the temperature of below deck equipment, and software Fluent can be utilized to carry out and calculated.
The heat source of below deck equipment heating includes three parts：In cabin high temperature heat source to the radiant heating of below deck equipment, equipment from
Body fever, air heat the heat conduction of below deck equipment.
By research, computational methods there are two types of the hot-fluids below deck equipment, the calculating knot of both analysis methods are loaded
Fruit is consistent, and visual feelings are selected.
This patent uses the User Defined interface that Fluent softwares provide, and by writing, program will " load be set in cabin
The language that calculating thinking, the computational methods of standby upper hot-fluid " are converted into Fluent identifications is embedded into software, controls entire calculate
Process.
Two kinds of computational methods of " hot-fluid of the load below deck equipment " are as follows：
(1) hot-fluid of the load below deck equipment is：
Q(w/m2Net radiation hot-fluid (Radiation Heat Flux) of the)=high temperature heat source to below deck equipment
+ below deck equipment self-heating hot-fluid
+ air conduction hot-fluid
In its middle deck high temperature heat source to the net radiation hot-fluid (Radiation Heat Flux) of below deck equipment by step 1.3
First method obtains, and the User Defined interface provided using Fluent, bespoke program is by (temperature, net radiation hot-fluid)
Database is loaded according to coordinate on equipment wall surface, and the net radiation hot-fluid of different moments can be by writing program to equipment wall surface temperature
The biquadratic interpolation of degree obtains.
Below deck equipment itself hot-fluid is provided by equipment development unit.
Air conduction hot-fluid is obtained using the engineering method of one-dimensional linear heat transfer between high temperature heat source and below deck equipment wall surface.
(2) hot-fluid of the load below deck equipment is：
Q(w/m2Radiant heat flux (the Absorbed that below deck equipment absorbs when)=high temperature heat source irradiates below deck equipment
Radiation Flux)
Self-heating hot-fluid in+cabin
+ air conduction hot-fluid
Since equipment itself high temperature is to the hot-fluid of external radiation
The radiant heat flux (Absorbed Radiation Flux) that wherein below deck equipment absorbs is by second of side of step 1.3
Method obtains, and the air conduction hot-fluid between high temperature heat source and below deck equipment wall surface is obtained using the engineering method of one-dimensional linear heat transfer
, since the high temperature of equipment itself obtains (ε σ T to the hot-fluid of external radiation using grey-body radiation formula4)。
The User Defined interface provided using Fluent writes the language that the above thinking is transformed into Fluent identifications by program
Speech load is in entire calculating process.
Step 3：It analyzes below deck equipment temperature and rises mechanism, propose the major measure of control below deck equipment Wen Sheng, to improve in cabin
Foundation is instructed in environment proposition
Step 3.1 analyzes below deck equipment temperature and rises mechanism
Using the method for step 2, for only consideration high temperature heat source radiation, consideration high temperature heat source radiation+self-heating, examine
Consider high temperature heat source radiation+self-heating+air conduction these three states, respectively the maximum temperature on analytical equipment surface.By right
Than the maximum temperature on these three status devices surfaces, the principal element and secondary cause that cause equipment Wen Sheng are judged.Fig. 1 is different
Inertial navigation under heat exchange approach and electric control box temperature.
It can find that electromagnetic radiation is the principal element for causing inertial navigation and electric control box overtemperature.
Step 3.2 proposes the major measure of control below deck equipment Wen Sheng, for improving below deck equipment environment
For the principal element and secondary cause for causing equipment Wen Sheng of 3.1 analyses, propose that control device Wen Sheng's is main
Measure is limitation principal element, and then improves below deck equipment environment.
It is electromagnetic radiation usually to cause the principal element of equipment Wen Sheng, to improve thermal environment in cabin, it is ensured that below deck equipment is not
Overtemperature need to take measures to reduce radiation of the battery to equipment, for example increase thermal baffle among battery and equipment.
As above it is directed to that a kind of embodiment describes and/or the feature that shows can be in a manner of same or similar at one or more
It is used in a number of other embodiments, and/or the feature in other embodiments is combined or substitutes with the feature in other embodiments
It uses.
It should be emphasized that term "comprises/comprising" refers to the presence of feature, one integral piece, step or component when being used herein, but simultaneously
It is not excluded for the presence or additional of one or more other features, one integral piece, step, component or combinations thereof.
The device and method more than present invention can be by hardware realization, can also be by combination of hardware software realization.The present invention
It is related to such computer-readable program, when the program is performed by logical block, the logical block can be made to realize above
The device or component parts, or the logical block is made to realize various method or steps described above.The invention further relates to
Storage medium for storing procedure above, such as hard disk, disk, CD, DVD, flash memory.
The many features and advantage of these embodiments are clear according to the detailed description, therefore appended claims are intended to
Cover all these feature and advantage of these embodiments fallen into its true spirit and range.Further, since this field
Technical staff is readily apparent that many modifications and changes, therefore is not meant to the embodiment of the present invention being limited to illustrated and description essence
Really structurally and operationally, but all suitable modifications and the equivalent fallen within the scope of its can be covered.
Unspecified part of the present invention is known to the skilled person technology.
Claims (1)
1. a kind of analysis method for hypersonic aircraft below deck equipment radiation/phenomenon of Heat, which is characterized in that this method
Include the following steps：
It determines and the high temperature heat source of radiant heating is generated to below deck equipment and obtains the temperature of high temperature heat source；
The grid that high temperature heat source calculates below deck equipment radiant heat transfer amount is generated, which only includes air-grid, and normal direction is adjacent
Size difference between grid is less than 1.5~3 times；
Carry out high temperature heat source using the grid to calculate the radiant heat transfer amount of below deck equipment, high temperature is analyzed using radiation patterns
The radiant heat flux that below deck equipment absorbs when heat source irradiates the below deck equipment of different temperatures is obtained and is absorbed under below deck equipment different temperatures
The database of radiant heat flux, the database include corresponding between below deck equipment node coordinate, wall temperature and absorption radiant heat flux
Relationship；
The heat transfer grid of below deck equipment is generated, which only includes structural thermal grid, and the size difference between adjacent mesh is less than 1.5
~3 times；
It determines that the self-heating power of below deck equipment, the power are only used for self-heating and elevate the temperature, is not used in equipment work；
Carry out first order below deck equipment Three-dimensional Heat-transfer temperature computation using the structural thermal grid, is set in the first order cabin
Standby Three-dimensional Heat-transfer temperature computation considers high temperature heat source radiation, equipment self-heating, air conduction, the outside spoke of equipment itself high temperature
It penetrates, the net hot-fluid of below deck equipment outer surface includes radiant heat flux, below deck equipment self-heating hot-fluid, sky that it absorbs high temperature heat source
Hot-fluid of itself high temperature of gas heat conduction heat flux, equipment to external radiation；The radiant heat flux that below deck equipment outer surface absorbs is cabin when calculating
Each node on interior device outer surface is in each respective temperature of time step extract real-time, then from the absorption radiant heat flux
Lane database extracts corresponding hot-fluid, the radiant heat flux absorbed at respective temperature load is obtained on this node, below deck equipment
Self-heating hot-fluid is self-heating power divided by surface area, and air conduction hot-fluid uses the engineering method of one-dimensional linear heat transfer
It obtains, equipment itself high temperature is obtained to the hot-fluid of external radiation using grey-body radiation formula；It is warmed in height using heat transfer model analysis
Source radiation heating, equipment self-heating, air conduction, temperature from equipment itself high temperature to below deck equipment under the comprehensive function of external radiation
Degree, obtains the maximum temperature of equipment surface；
Carry out second level below deck equipment Three-dimensional Heat-transfer temperature computation using the structural thermal grid, is set in the second level cabin
Standby Three-dimensional Heat-transfer temperature computation considers high temperature heat source radiation, equipment self-heating, equipment itself high temperature to external radiation, below deck equipment
The net hot-fluid of outer surface includes radiant heat flux, below deck equipment self-heating hot-fluid, equipment itself high temperature that it absorbs high temperature heat source
To the hot-fluid of external radiation；The radiant heat flux that below deck equipment outer surface absorbs is each node below deck equipment outer surface when calculating
Corresponding hot-fluid is extracted in each respective temperature of time step extract real-time, then from the absorption radiant heat flux lane database,
The radiant heat flux absorbed at respective temperature load is obtained on this node, below deck equipment self-heating hot-fluid is self-heating work(
Rate divided by surface area, equipment itself high temperature are obtained to the hot-fluid of external radiation using grey-body radiation formula；It is analyzed using heat transfer model
The temperature of below deck equipment under the comprehensive function of high temperature heat source radiant heating, equipment self-heating, equipment itself high temperature to external radiation
Degree, obtains the maximum temperature of equipment surface；
Carry out third level below deck equipment Three-dimensional Heat-transfer temperature computation using the structural thermal grid, is set in the third level cabin
Standby Three-dimensional Heat-transfer temperature computation considers high temperature heat source radiation, equipment itself high temperature to external radiation, the net heat of below deck equipment outer surface
Stream comprising it absorb the radiant heat flux of high temperature heat source, hot-fluid from equipment itself high temperature to external radiation；Below deck equipment outer surface absorbs
Radiant heat flux be each node when calculating below deck equipment outer surface in each respective temperature of time step extract real-time,
Corresponding hot-fluid is extracted from the absorption radiant heat flux lane database again, the radiant heat flux absorbed at respective temperature is loaded at this
It is obtained on node, equipment itself high temperature is obtained to the hot-fluid of external radiation using grey-body radiation formula；Existed using heat transfer model analysis
Itself high temperature of high temperature heat source radiant heating, equipment obtains equipment surface to the temperature of below deck equipment under the comprehensive function of external radiation
Maximum temperature；
Mechanism is risen using equipment surface maximum temperature analytical equipment temperature in the case of three kinds of above-mentioned calculating, proposes to improve below deck equipment
The major measure of thermal environment, influence of the air conduction to equipment maximum temperature are " to be passed by the first order below deck equipment three-dimensional
Thermel calculates the equipment maximum temperature obtained " it subtracts " by second level below deck equipment Three-dimensional Heat-transfer temperature computation acquisition
Equipment maximum temperature ", influence of the equipment self-heating to equipment maximum temperature is " it is three-dimensional to pass through the second level below deck equipment
Heat transfer temperature calculates the equipment maximum temperature obtained " it subtracts and " is obtained by the third level below deck equipment Three-dimensional Heat-transfer temperature computation
The equipment maximum temperature obtained ", influence of the high temperature heat source to equipment maximum temperature are to pass through the third level below deck equipment three-dimensional to pass
Thermel calculates the equipment maximum temperature obtained, compares air conduction, equipment self-heating, these three factors of high temperature heat source in cabin
Influence to equipment maximum temperature, it is to cause the principal element of equipment high temperature to influence maximum factor, and other factors are to cause to set
The secondary cause of standby Wen Sheng, control device Wen Sheng, the major measure for improving thermal environment in cabin are limitation principal elements.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710306478.0A CN108304596B (en) | 2017-05-04 | 2017-05-04 | Analysis method for radiation/heat transfer phenomenon of equipment in cabin of hypersonic aircraft |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710306478.0A CN108304596B (en) | 2017-05-04 | 2017-05-04 | Analysis method for radiation/heat transfer phenomenon of equipment in cabin of hypersonic aircraft |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109918765A (en) * | 2019-03-04 | 2019-06-21 | 北京空天技术研究所 | Thermal environment couples Precise computation in a kind of high-speed aircraft cabin |
| CN110008547A (en) * | 2019-03-25 | 2019-07-12 | 山东省科学院海洋仪器仪表研究所 | A kind of analysis of Heat Transfer method of underwater data acquisition cabin DC power supplier |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8571838B1 (en) * | 2010-08-04 | 2013-10-29 | The Boeing Company | Analysis of fluid flow over a surface |
| CN105956286A (en) * | 2016-05-06 | 2016-09-21 | 北京航空航天大学 | Prediction method of forecabin thermal protection system whole trajectory temperature boundary of hypersonic velocity aircraft |
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2017
- 2017-05-04 CN CN201710306478.0A patent/CN108304596B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8571838B1 (en) * | 2010-08-04 | 2013-10-29 | The Boeing Company | Analysis of fluid flow over a surface |
| CN105956286A (en) * | 2016-05-06 | 2016-09-21 | 北京航空航天大学 | Prediction method of forecabin thermal protection system whole trajectory temperature boundary of hypersonic velocity aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109918765A (en) * | 2019-03-04 | 2019-06-21 | 北京空天技术研究所 | Thermal environment couples Precise computation in a kind of high-speed aircraft cabin |
| CN109918765B (en) * | 2019-03-04 | 2023-06-20 | 北京空天技术研究所 | High-speed aircraft cabin thermal environment coupling fine calculation method |
| CN110008547A (en) * | 2019-03-25 | 2019-07-12 | 山东省科学院海洋仪器仪表研究所 | A kind of analysis of Heat Transfer method of underwater data acquisition cabin DC power supplier |
| CN110008547B (en) * | 2019-03-25 | 2022-11-29 | 山东省科学院海洋仪器仪表研究所 | Heat transfer analysis method for direct-current power supply module of underwater data acquisition cabin |
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|---|---|
| CN108304596B (en) | 2021-06-08 |
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