FR2982024B1 - Procede de calcul de pression dynamique au niveau d'une surface d'aeronef - Google Patents

Procede de calcul de pression dynamique au niveau d'une surface d'aeronef

Info

Publication number
FR2982024B1
FR2982024B1 FR1159838A FR1159838A FR2982024B1 FR 2982024 B1 FR2982024 B1 FR 2982024B1 FR 1159838 A FR1159838 A FR 1159838A FR 1159838 A FR1159838 A FR 1159838A FR 2982024 B1 FR2982024 B1 FR 2982024B1
Authority
FR
France
Prior art keywords
dynamic pressure
aircraft surface
calculating dynamic
calculating
aircraft
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.)
Expired - Fee Related
Application number
FR1159838A
Other languages
English (en)
Other versions
FR2982024A1 (fr
Inventor
Benoit Calmels
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1159838A priority Critical patent/FR2982024B1/fr
Priority to US13/661,958 priority patent/US9187187B2/en
Publication of FR2982024A1 publication Critical patent/FR2982024A1/fr
Application granted granted Critical
Publication of FR2982024B1 publication Critical patent/FR2982024B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/15—Vehicle, aircraft or watercraft design
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/20—Design optimisation, verification or simulation
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Fluid Mechanics (AREA)
  • Automation & Control Theory (AREA)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR1159838A 2011-10-28 2011-10-28 Procede de calcul de pression dynamique au niveau d'une surface d'aeronef Expired - Fee Related FR2982024B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1159838A FR2982024B1 (fr) 2011-10-28 2011-10-28 Procede de calcul de pression dynamique au niveau d'une surface d'aeronef
US13/661,958 US9187187B2 (en) 2011-10-28 2012-10-26 Method of calculating dynamic pressure at the level of an aircraft surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1159838A FR2982024B1 (fr) 2011-10-28 2011-10-28 Procede de calcul de pression dynamique au niveau d'une surface d'aeronef

Publications (2)

Publication Number Publication Date
FR2982024A1 FR2982024A1 (fr) 2013-05-03
FR2982024B1 true FR2982024B1 (fr) 2014-06-13

Family

ID=45351063

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1159838A Expired - Fee Related FR2982024B1 (fr) 2011-10-28 2011-10-28 Procede de calcul de pression dynamique au niveau d'une surface d'aeronef

Country Status (2)

Country Link
US (1) US9187187B2 (fr)
FR (1) FR2982024B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109033548B (zh) * 2018-07-03 2020-07-07 中国空气动力研究与发展中心高速空气动力研究所 一种计算槽壁边界条件主要系数的拟合方法
CN111539063B (zh) * 2020-03-26 2023-12-15 中国航天空气动力技术研究院 一种过渡流区飞行器缝隙热流及防热材料的确定方法
CN111695193B (zh) * 2020-05-11 2021-01-22 上海机电工程研究所 一种全局相关三维气动力数学模型的建模方法及系统
CN112287455B (zh) * 2020-10-29 2024-06-21 西北工业大学 一种复杂飞机构型气动载荷批量提取方法
CN114018532B (zh) * 2021-11-09 2023-02-28 中国空气动力研究与发展中心超高速空气动力研究所 一种高超声速风洞连续变总压的试验方法
CN114061896B (zh) * 2021-11-17 2023-04-25 中国空气动力研究与发展中心超高速空气动力研究所 升力体通气模型内阻测量试验数据处理方法
CN115628877A (zh) * 2022-12-20 2023-01-20 中国航空工业集团公司沈阳空气动力研究所 一种用于翼型试验的连续扫描式尾迹测量方法和装置
CN117852184B (zh) * 2024-01-09 2024-07-23 溧阳气动创新研究院有限公司 飞行器多环境下空气动力载荷等效预测分析方法及系统

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7146299B2 (en) * 2002-08-16 2006-12-05 The Boeing Company Adjustable simulation vehicle capabilities
EP1828883B1 (fr) * 2004-10-15 2015-12-23 Bell Helicopter Textron, Inc. Procede destine a la conception d'un aeronef
US8280663B2 (en) * 2007-10-31 2012-10-02 Airbus Operations S.L. Methods and systems for assisting in the design of mobile surfaces of objects
JP5354659B2 (ja) * 2009-04-06 2013-11-27 独立行政法人 宇宙航空研究開発機構 流体力分布計測方法及び計測装置
FR2944623B1 (fr) * 2009-04-21 2011-06-10 Airbus France Procede et outil de simulation du comportement aerodynamique d'un aeronef en vol au voisinage du sol
FR2944896B1 (fr) * 2009-04-24 2011-07-08 Airbus France Procede de prediction du comportement aerodynamique d'une structure d'un aeronef
FR2946430B1 (fr) * 2009-06-03 2011-08-26 Airbus France Procede et dispositif pour determiner des charges critiques dues a un tremblement sur une structure d'un avion.

Also Published As

Publication number Publication date
US20130191087A1 (en) 2013-07-25
US9187187B2 (en) 2015-11-17
FR2982024A1 (fr) 2013-05-03

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