AU2003239764A8 - Method and device for determining the aerodynamic wall shear stresses on the surface of a body, around which air flows - Google Patents

Method and device for determining the aerodynamic wall shear stresses on the surface of a body, around which air flows

Info

Publication number: AU2003239764A8
Authority: AU; Australia
Prior art keywords: determining; around; air flows; shear stresses; wall shear
Prior art date: 2002-06-07
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

AU2003239764A

Other versions

AU2003239764A1 (en

Inventor

Ole Trinks

Bernd Schulze

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 Defence and Space GmbH

Original Assignee

EADS Deutschland GmbH

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.)

2002-06-07

Filing date

2003-06-03

Publication date

2003-12-22

2003-06-03 Application filed by EADS Deutschland GmbH filed Critical EADS Deutschland GmbH

2003-12-22 Publication of AU2003239764A1 publication Critical patent/AU2003239764A1/en

2003-12-22 Publication of AU2003239764A8 publication Critical patent/AU2003239764A8/en

Status Abandoned legal-status Critical Current

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
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing

Landscapes

Physics & Mathematics (AREA)
Fluid Mechanics (AREA)
General Physics & Mathematics (AREA)
Radiation Pyrometers (AREA)
Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Investigating Or Analyzing Materials Using Thermal Means (AREA)

AU2003239764A 2002-06-07 2003-06-03 Method and device for determining the aerodynamic wall shear stresses on the surface of a body, around which air flows Abandoned AU2003239764A1 (en)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
DE2002125616 DE10225616B4 (en)	2002-06-07	2002-06-07	Method and device for determining the aerodynamic wall shear stresses on the surface of a body flowing around
DE10225616.0		2002-06-07
PCT/DE2003/001797 WO2003104769A2 (en)	2002-06-07	2003-06-03	Method and device for determining the aerodynamic wall shear stresses on the surface of a body, around which air flows

Publications (2)

Publication Number	Publication Date
AU2003239764A1 AU2003239764A1 (en)	2003-12-22
AU2003239764A8 true AU2003239764A8 (en)	2003-12-22

Family

ID=29718916

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
AU2003239764A Abandoned AU2003239764A1 (en)	2002-06-07	2003-06-03	Method and device for determining the aerodynamic wall shear stresses on the surface of a body, around which air flows

Country Status (4)

Country	Link
EP (1)	EP1514086A2 (en)
AU (1)	AU2003239764A1 (en)
DE (1)	DE10225616B4 (en)
WO (1)	WO2003104769A2 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102005018169A1 (en) *	2005-04-19	2006-11-02	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Method for determining pressure distribution over a surface and pressure sensitive paint for use thereby
DE102007054933A1 (en) *	2007-11-17	2009-05-28	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Wall shear stress measuring method for e.g. air craft, involves determining displacement of reference point as result of subjecting sample with flow of fluid, and determining stress under consideration of determined layer thickness
CN106768820A (en) *	2017-01-12	2017-05-31	中国人民解放军63820部队吸气式高超声速技术研究中心	The test method of scramjet engine wall surface temperature effect study in impulse wind tunnel
CN107543648B (en) *	2017-07-17	2019-06-04	西北工业大学	High temperature shear stress sensor based on double F-P cavity and preparation method thereof
CN112268684B (en) *	2020-12-14	2021-03-19	中国空气动力研究与发展中心低速空气动力研究所	Variable azimuth angle surface pressure measuring system and method for low-speed wind tunnel rotor model
CN113834625B (en) *	2021-10-13	2022-02-25	中国空气动力研究与发展中心低速空气动力研究所	Aircraft model surface pressure measuring method and system
CN114199499B (en) *	2022-02-16	2022-04-22	中国空气动力研究与发展中心超高速空气动力研究所	Heat storage element for large-flow high-temperature high-pressure high-speed gas environment

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3514801A1 (en) *	1985-04-24	1986-10-30	Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln	METHOD AND DEVICE FOR DETERMINING THE WALL SHEAR TENSION ON MODELS AND OTHER FLOWED BODIES
DE4134313C2 (en) *	1991-10-17	1997-03-06	Daimler Benz Aerospace Ag	Infrared measuring method and measuring arrangement
US5438879A (en) *	1993-03-16	1995-08-08	The United States Of America Represented By The Administrator Of The National Aeronautics And Space Administration	Method for measuring surface shear stress magnitude and direction using liquid crystal coatings
US5612492A (en) *	1995-06-07	1997-03-18	Mcdonnell Douglas Corporation	Formulations and method of use of pressure sensitive paint
US5963310A (en) *	1997-06-11	1999-10-05	The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration	Surface imaging skin friction instrument and method

2002
- 2002-06-07 DE DE2002125616 patent/DE10225616B4/en not_active Expired - Fee Related
2003
- 2003-06-03 WO PCT/DE2003/001797 patent/WO2003104769A2/en not_active Ceased
- 2003-06-03 AU AU2003239764A patent/AU2003239764A1/en not_active Abandoned
- 2003-06-03 EP EP03732239A patent/EP1514086A2/en not_active Withdrawn

Also Published As

Publication number	Publication date
AU2003239764A1 (en)	2003-12-22
EP1514086A2 (en)	2005-03-16
DE10225616A1 (en)	2004-01-08
DE10225616B4 (en)	2004-09-09
WO2003104769A3 (en)	2004-02-12
WO2003104769A2 (en)	2003-12-18

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Legal Events

Date	Code	Title	Description
2005-02-24	MK6	Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase