CN105539863B - Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method - Google Patents
Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method Download PDFInfo
- Publication number
- CN105539863B CN105539863B CN201610067619.3A CN201610067619A CN105539863B CN 105539863 B CN105539863 B CN 105539863B CN 201610067619 A CN201610067619 A CN 201610067619A CN 105539863 B CN105539863 B CN 105539863B
- Authority
- CN
- China
- Prior art keywords
- support plate
- flow field
- air intake
- intake duct
- precursor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0253—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
- B64D2033/026—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
Abstract
Description
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610067619.3A CN105539863B (en) | 2016-01-29 | 2016-01-29 | Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610067619.3A CN105539863B (en) | 2016-01-29 | 2016-01-29 | Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method |
Publications (2)
Publication Number | Publication Date |
---|---|
CN105539863A CN105539863A (en) | 2016-05-04 |
CN105539863B true CN105539863B (en) | 2017-06-13 |
Family
ID=55819519
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610067619.3A Active CN105539863B (en) | 2016-01-29 | 2016-01-29 | Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN105539863B (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111339672B (en) * | 2020-03-02 | 2021-06-08 | 上海索辰信息科技股份有限公司 | Method for analyzing aerodynamic thermal simulation of shock wave at front edge of air inlet channel |
CN113236424B (en) * | 2021-06-22 | 2022-07-05 | 西安航天动力研究所 | Double-lower-side rear supersonic air inlet |
CN113250821B (en) * | 2021-06-30 | 2022-06-07 | 中国人民解放军国防科技大学 | Hypersonic air inlet layout for annular combustion chamber |
CN114379812B (en) * | 2021-12-28 | 2023-04-28 | 南京航空航天大学 | High-speed precursor/compression surface pneumatic design method with controllable spanwise pressure distribution |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5337975A (en) * | 1992-02-28 | 1994-08-16 | Rockwell International Corporation | Breathing system for hypersonic aircraft |
US7866599B2 (en) * | 2006-02-14 | 2011-01-11 | Lockheed-Martin Corporation | Integrated inward turning inlets and nozzles for hypersonic air vehicles |
CN101392685B (en) * | 2008-10-29 | 2010-06-09 | 南京航空航天大学 | Internal waverider hypersonic inlet and design method based on random shock form |
CN103662087B (en) * | 2013-12-11 | 2015-07-15 | 厦门大学 | Hypersonic aerocraft and air inlet internal and external waverider integrated design method |
CN104895676A (en) * | 2015-04-14 | 2015-09-09 | 中国科学院力学研究所 | High supersonic speed variable cross section air intake duct and design method thereof |
CN105151306B (en) * | 2015-09-29 | 2017-02-22 | 厦门大学 | Method of integrally designing forebody and air intake duct of cone configuration hypersonic flight vehicle |
CN105151307B (en) * | 2015-10-08 | 2017-02-01 | 北京航空航天大学 | Method for cutting Mach surface of hypersonic aircraft with forebody/air inlet pipeline in integrated design |
-
2016
- 2016-01-29 CN CN201610067619.3A patent/CN105539863B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN105539863A (en) | 2016-05-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN112340014B (en) | Inner-outer flow decoupling double-waverider high-speed air suction type aircraft and generation method thereof | |
CN105539863B (en) | Hypersonic aircraft precursor, air intake duct and support plate integrated pneumatic layout method | |
CN105947230B (en) | A kind of Waverider and the method for designing of air intake duct integration configuration | |
CN105775158B (en) | Hypersonic slender bodies aircraft in three-dimensional with rotating into air passage integrated design method | |
CN106837549B (en) | The design method of interior parallel hypersonic binary channels air intake duct | |
CN105151306B (en) | Method of integrally designing forebody and air intake duct of cone configuration hypersonic flight vehicle | |
CN106741976B (en) | A kind of mimetic design method of waverider forebody derived air intake duct integration configuration | |
CN106837550A (en) | The method for designing of hypersonic triple channel air intake duct | |
CN104908975B (en) | Aircraft fore-body and internal waverider-derived hypersonic inlet integrated design method | |
CN107089341B (en) | With aircraft integrated hypersonic inlet external compression face design method | |
CN105667812A (en) | Waverider integration design method for hypersonic aircraft forebody, air inlet and wing | |
CN106250597A (en) | Air flue design method is rotated in a kind of three-dimensional flowing to suction completely | |
US20070181743A1 (en) | Method for streamline traced external compression inlet | |
CN110182380B (en) | Hypersonic speed internal and external flow integrated design method based on typical internal rotation air inlet channel | |
CN109250144A (en) | Method for designing osculating cone waverider with directly controllable sweepback angle and upper/lower dihedral angles | |
CN110304267B (en) | Hypersonic aircraft design method and system | |
CN107672821B (en) | Variable Mach number parallel wide-speed-range waverider aircraft design method based on osculating cone theory | |
CN105221264A (en) | Based on closely boring the bump inlet design method leading rider theory | |
CN107867387A (en) | Outflow Waverider aircraft layout in a kind of | |
CN104975950A (en) | Method for determining binary hypersonic inlet passage based on appointed wall pressure distribution | |
CN106777828A (en) | The controllable inside and outside rider integrated design method of wall pressure | |
CN111003196B (en) | Full-wave-rider aircraft and design method and system thereof | |
CN110210096B (en) | Design method of variable-section three-dimensional internal-contraction air inlet channel matched with curved cone bullet body | |
CN105059531B (en) | Osculating cone waverider with curve head and controllable sweepback angle | |
CN108829961B (en) | Nacelle-engine body matching design method adopting back-support engine wing body fusion layout |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CB03 | Change of inventor or designer information |
Inventor after: Wang Chengpeng Inventor after: Cheng Chuan Inventor after: Xue Longsheng Inventor after: Yan Lingfeng Inventor after: Tian Xuang Inventor after: Ni Shiyang Inventor after: Cheng Keming Inventor before: Wang Chengpeng Inventor before: Xue Longsheng Inventor before: Cheng Chuan Inventor before: Yan Lingfeng Inventor before: Tian Xuang Inventor before: Ni Shiyang Inventor before: Cheng Keming |
|
CB03 | Change of inventor or designer information |