FR2952454B1 - METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE - Google Patents

METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE

Info

Publication number
FR2952454B1
FR2952454B1 FR0957878A FR0957878A FR2952454B1 FR 2952454 B1 FR2952454 B1 FR 2952454B1 FR 0957878 A FR0957878 A FR 0957878A FR 0957878 A FR0957878 A FR 0957878A FR 2952454 B1 FR2952454 B1 FR 2952454B1
Authority
FR
France
Prior art keywords
aerodynamic
simulating
aircraft
tool
variable array
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
FR0957878A
Other languages
French (fr)
Other versions
FR2952454A1 (en
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 FR0957878A priority Critical patent/FR2952454B1/en
Priority to PCT/FR2010/052371 priority patent/WO2011055085A2/en
Publication of FR2952454A1 publication Critical patent/FR2952454A1/en
Application granted granted Critical
Publication of FR2952454B1 publication Critical patent/FR2952454B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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)
  • Theoretical Computer Science (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • General Engineering & Computer Science (AREA)
  • Evolutionary Computation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Computational Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR0957878A 2009-11-06 2009-11-06 METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE Expired - Fee Related FR2952454B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0957878A FR2952454B1 (en) 2009-11-06 2009-11-06 METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE
PCT/FR2010/052371 WO2011055085A2 (en) 2009-11-06 2010-11-04 Method and tool for simulating the aerodynamic behaviour of an aerodynamic element of an aircraft having a variable sweep angle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0957878A FR2952454B1 (en) 2009-11-06 2009-11-06 METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE

Publications (2)

Publication Number Publication Date
FR2952454A1 FR2952454A1 (en) 2011-05-13
FR2952454B1 true FR2952454B1 (en) 2011-12-23

Family

ID=42289094

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0957878A Expired - Fee Related FR2952454B1 (en) 2009-11-06 2009-11-06 METHOD AND TOOL FOR SIMULATING THE AERODYNAMIC BEHAVIOR OF AERODYNAMIC ELEMENT OF AN AIRCRAFT HAVING A VARIABLE ARRAY ANGLE

Country Status (2)

Country Link
FR (1) FR2952454B1 (en)
WO (1) WO2011055085A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107766673B (en) * 2017-11-10 2018-07-31 中国人民解放军国防科技大学 Radius-controllable parameterized three-dimensional leading edge passivation design method
CN110457860A (en) * 2019-08-22 2019-11-15 中国商用飞机有限责任公司北京民用飞机技术研究中心 The automatically generating of grid, device, equipment and storage medium
CN111174645B (en) * 2020-01-17 2022-04-15 西安智芯通达科技有限公司 Missile wing active flutter suppression method based on L1 adaptive control algorithm
CN111460591A (en) * 2020-03-31 2020-07-28 合肥工业大学 Large uncertainty crane system amplitude-variation angle prediction method based on subinterval theory
CN112214834B (en) * 2020-09-11 2024-02-06 北京空间飞行器总体设计部 Axisymmetric aircraft pneumatic database establishment method

Also Published As

Publication number Publication date
WO2011055085A2 (en) 2011-05-12
WO2011055085A3 (en) 2011-07-28
FR2952454A1 (en) 2011-05-13

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