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 ANGLEInfo
- 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
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)
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)
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 |
-
2009
- 2009-11-06 FR FR0957878A patent/FR2952454B1/en not_active Expired - Fee Related
-
2010
- 2010-11-04 WO PCT/FR2010/052371 patent/WO2011055085A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2011055085A3 (en) | 2011-07-28 |
WO2011055085A2 (en) | 2011-05-12 |
FR2952454A1 (en) | 2011-05-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
ST | Notification of lapse |
Effective date: 20210705 |