AU2001284218A1 - Wind tunnel testing - Google Patents

Wind tunnel testing

Info

Publication number
AU2001284218A1
AU2001284218A1 AU2001284218A AU8421801A AU2001284218A1 AU 2001284218 A1 AU2001284218 A1 AU 2001284218A1 AU 2001284218 A AU2001284218 A AU 2001284218A AU 8421801 A AU8421801 A AU 8421801A AU 2001284218 A1 AU2001284218 A1 AU 2001284218A1
Authority
AU
Australia
Prior art keywords
wind tunnel
tunnel testing
model
testing
vibration
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.)
Abandoned
Application number
AU2001284218A
Inventor
Thomas Mark Gibson
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Publication of AU2001284218A1 publication Critical patent/AU2001284218A1/en
Abandoned legal-status Critical Current

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
    • G01M9/08—Aerodynamic models

Abstract

A wind tunnel model for wind tunnel testing having an additional mass mounted on the model via vibration absorbing material to dampen model vibration.
AU2001284218A 2000-09-07 2001-08-31 Wind tunnel testing Abandoned AU2001284218A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB0021925.3A GB0021925D0 (en) 2000-09-07 2000-09-07 Wind tunnel testing
GB0021925 2000-09-07
PCT/GB2001/003904 WO2002021097A1 (en) 2000-09-07 2001-08-31 Wind tunnel testing

Publications (1)

Publication Number Publication Date
AU2001284218A1 true AU2001284218A1 (en) 2002-03-22

Family

ID=9899000

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001284218A Abandoned AU2001284218A1 (en) 2000-09-07 2001-08-31 Wind tunnel testing

Country Status (8)

Country Link
US (1) US7127942B2 (en)
EP (1) EP1315956B1 (en)
AT (1) ATE421084T1 (en)
AU (1) AU2001284218A1 (en)
CA (1) CA2421453C (en)
DE (1) DE60137434D1 (en)
GB (1) GB0021925D0 (en)
WO (1) WO2002021097A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2339317B1 (en) * 2008-04-30 2011-03-11 Airbus Operations, S.L. AERODYNAMIC INTERFERENCE MINIMUM SUPPORT-MAQUETTE ASSEMBLY FOR TRIALS IN A TRANSONIC REGIME IN WIND TUNNEL.
US9052250B1 (en) 2012-05-04 2015-06-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of calibrating a force balance
US8783098B2 (en) * 2012-05-14 2014-07-22 The Boeing Company Wind tunnel model measuring system and method
US9541149B2 (en) * 2014-09-04 2017-01-10 The Boeing Company Translational tuned mass damper with continuously adjustable damping characteristics for application to high speed wind tunnel testing
US10060823B2 (en) * 2016-02-19 2018-08-28 The Boeing Company Miniaturized tuned mass damper for application to high speed wind tunnel testing
CN105758611A (en) * 2016-03-07 2016-07-13 中国空气动力研究与发展中心高速空气动力研究所 Impact resisting device for wind-tunnel balance
US10309867B2 (en) 2016-08-15 2019-06-04 The Boeing Company Variable spring-constant tuned mass damper
US10460588B2 (en) 2016-09-06 2019-10-29 The Boeing Company Systems and methods for wind tunnel operation
US10533921B2 (en) 2016-12-02 2020-01-14 The Boeing Company Tunable mass damper characterization test stand
US11169048B2 (en) 2019-09-16 2021-11-09 The Boeing Company Wind tunnel sting, wind tunnel sting damper, and method therefor

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1084260A (en)
US3514054A (en) 1967-06-05 1970-05-26 United Aircraft Corp Vibration isolation system
US3572112A (en) * 1969-06-30 1971-03-23 Nasa Dynamic vibration absorber
US3587306A (en) * 1969-11-06 1971-06-28 Max B Bryan Wind tunnel model damper
US4327581A (en) * 1980-04-30 1982-05-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Metric half-span model support system
US4372158A (en) * 1981-06-17 1983-02-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aeroelastic instability stoppers for wind tunnel models
US4475385A (en) * 1983-03-31 1984-10-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Model mount system for testing flutter
US4809553A (en) * 1987-07-16 1989-03-07 Dynamic Engineering Inc. Flutter exciter
IL86471A (en) * 1988-05-23 1991-08-16 Israel Aircraft Ind Ltd Apparatus for dissipating shock-wave energy experienced by a test model
US4862739A (en) * 1988-06-16 1989-09-05 Rockwell International Corporation Wind tunnel model support mechanism
JPH0875596A (en) * 1994-09-09 1996-03-22 Mitsubishi Heavy Ind Ltd Stinger for wind tunnel test
DE19549339C1 (en) * 1995-04-07 1996-10-24 Europ Transonic Windtunnel Model carrier for wind tunnel models
US5663497A (en) * 1996-07-22 1997-09-02 Mole; Philip J. Six component wind tunnel balance
US6021770A (en) * 1997-07-28 2000-02-08 Arvid A. Ames Bow stabilizer with game finder
AU2001297537A1 (en) * 2000-11-06 2002-10-08 The Johns Hopkins University Rapid prototype wind tunnel model and method of making same
JP4446608B2 (en) * 2001-01-09 2010-04-07 本田技研工業株式会社 Wind tunnel test model

Also Published As

Publication number Publication date
US20030177825A1 (en) 2003-09-25
GB0021925D0 (en) 2000-10-25
ATE421084T1 (en) 2009-01-15
DE60137434D1 (en) 2009-03-05
CA2421453C (en) 2007-08-14
WO2002021097A1 (en) 2002-03-14
EP1315956B1 (en) 2009-01-14
US7127942B2 (en) 2006-10-31
CA2421453A1 (en) 2002-03-14
EP1315956A1 (en) 2003-06-04

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