The use of 2-D adaptive wall test sections for 3-D flows

Author:

WEDEMEYER E.1,LAMARCHE L.2

Affiliation:

1. DFVLR, Goettingen, Federal Republic of Germany

2. Montreal, Universite, Montreal, Canada

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Fcrri,A., Raronti,P.; A Mcthotl for T r a n w n i c Wintl Tunncl Corrcctionc. A l A A Sournal, Vol. lI, pp.63-66, (1973)

2. Wetlctncyrr,E.; Wintl Tunnel Testing of I htcc Dnicnsion:lModel\ in Wind Tunncls w t hT n o Adaptive Walls. VKI T N 147, (1982)

3. Vcrtc,D.; Interfcrencc Reciducllc d a n \ unc Souff l c r e Trancconiquc a P a r o n Adaptec\ a un Ecoulcmcnt B d m e n s o n cl clans I 'Etudc d c I 'Ecoulement Autour d'un Gorp\ Ax 14yctriquc. Travail d e fin d'etudcs, Uniwrsite L l b cd e Bruxellec, (1982)

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Update on progress in adaptive wind tunnel wall technology;Progress in Aerospace Sciences;2004-04

2. A further study on adaptive wall strategy for half-model testing;13th Applied Aerodynamics Conference;1995-06-19

3. Residual interference and wind-tunnel wall adaptation;AIAA Journal;1990-10

4. Residual interference and wind tunnel wall adaptation;27th Aerospace Sciences Meeting;1989-01-09

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