FR2932883B1 - Procede hybride pour l'evaluation de l'effet de sol sur un aeronef - Google Patents

Procede hybride pour l'evaluation de l'effet de sol sur un aeronef

Info

Publication number
FR2932883B1
FR2932883B1 FR0803428A FR0803428A FR2932883B1 FR 2932883 B1 FR2932883 B1 FR 2932883B1 FR 0803428 A FR0803428 A FR 0803428A FR 0803428 A FR0803428 A FR 0803428A FR 2932883 B1 FR2932883 B1 FR 2932883B1
Authority
FR
France
Prior art keywords
aircraft
evaluating
hybrid method
flood effect
flood
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
Application number
FR0803428A
Other languages
English (en)
Other versions
FR2932883A1 (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 FR0803428A priority Critical patent/FR2932883B1/fr
Priority to US12/485,140 priority patent/US7926340B2/en
Publication of FR2932883A1 publication Critical patent/FR2932883A1/fr
Application granted granted Critical
Publication of FR2932883B1 publication Critical patent/FR2932883B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G01M9/02—Wind tunnels
    • 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
FR0803428A 2008-06-19 2008-06-19 Procede hybride pour l'evaluation de l'effet de sol sur un aeronef Active FR2932883B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0803428A FR2932883B1 (fr) 2008-06-19 2008-06-19 Procede hybride pour l'evaluation de l'effet de sol sur un aeronef
US12/485,140 US7926340B2 (en) 2008-06-19 2009-06-16 Hybrid method for estimating the ground effect on an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0803428A FR2932883B1 (fr) 2008-06-19 2008-06-19 Procede hybride pour l'evaluation de l'effet de sol sur un aeronef

Publications (2)

Publication Number Publication Date
FR2932883A1 FR2932883A1 (fr) 2009-12-25
FR2932883B1 true FR2932883B1 (fr) 2010-08-20

Family

ID=40351660

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0803428A Active FR2932883B1 (fr) 2008-06-19 2008-06-19 Procede hybride pour l'evaluation de l'effet de sol sur un aeronef

Country Status (2)

Country Link
US (1) US7926340B2 (fr)
FR (1) FR2932883B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2966951A1 (fr) * 2010-11-03 2012-05-04 Airbus Operations Sas Procede de simulation pour determiner des coefficients aerodynamiques d'un aeronef
CN102589840B (zh) * 2012-01-12 2014-04-16 清华大学 一种垂直或短距起降飞机地面效应试验系统
CN103364170A (zh) * 2013-07-05 2013-10-23 北京航空航天大学 气动弹性稳定性的地面模拟预测方法和系统
CN103398835B (zh) * 2013-08-21 2016-01-06 中国人民解放军国防科学技术大学 基于高超声速炮风洞的气膜冷却瞬态热流测试系统及方法
KR101549526B1 (ko) 2014-03-12 2015-09-03 국방과학연구소 지면 충돌방지 기능이 내장된 비행체 지면효과 시험장치
US11181934B1 (en) 2020-05-20 2021-11-23 Honeywell International Inc. Systems and methods for predicting ground effects along a flight plan

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3224265A (en) * 1962-05-07 1965-12-21 Aerojet General Co Method for determining aerodynamic influence coefficients of a wing
US3250121A (en) * 1964-01-31 1966-05-10 Conductron Corp Helicopter ground proximity indicator
US5089968A (en) * 1990-01-26 1992-02-18 The Boeing Company Ground effects compensated real time aircraft body angle of attack estimation
US5186415A (en) * 1990-05-14 1993-02-16 Qun Li Aircraft having means for controlling the ground effect flying altitude by sensing air pressure on the surface of the wing
US5457630A (en) * 1992-11-18 1995-10-10 Aers/Midwest, Inc. System for onboard lift analysis and apparatus therefor
US5781126A (en) * 1996-07-29 1998-07-14 Alliedsignal Inc. Ground proximity warning system and methods for rotary wing aircraft
RU2118269C1 (ru) * 1997-07-02 1998-08-27 Вячеслав Васильевич Колганов Аэродинамический профиль крыла экраноплана
AU5803901A (en) * 2000-05-18 2001-11-26 Ken R Allen Wing in ground effect vehicle with endplates
US6547181B1 (en) * 2002-05-29 2003-04-15 The Boeing Company Ground effect wing having a variable sweep winglet
FR2929724B1 (fr) * 2008-04-02 2010-04-30 Airbus France Procede pour la determination de la vitesse de sortie d'effet de sol d'un aeronef.
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

Also Published As

Publication number Publication date
FR2932883A1 (fr) 2009-12-25
US7926340B2 (en) 2011-04-19
US20090314076A1 (en) 2009-12-24

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