COMPUTATIONAL DESIGN OF LOW ASPECT RATIO WING-WINGLET CONFIGURATIONS FOR TRANSONIC WIND-TUNNEL TESTS

COMPUTATIONAL DESIGN OF LOW ASPECT RATIO WING-WINGLET CONFIGURATIONS FOR TRANSONIC WIND-TUNNEL TESTS

著者名:

Kuhiman, John M. ( WEST VIRGINIA UNIVERSITY )
Brown, Christopher K.

掲載資料名:

NASA Technical Reports

発行年:

1989

号:

NASA-CR-181939

通号:

G3/02 0252162

パート:

NAS 1.26:181939

ペーパー番号:

N90-17539

開始ページ:

1

終了ページ:

114

総ページ数:

114

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001426
論文注記:	NAG1-625

類似資料:

1 テクニカルペーパー COMPUTATIONAL DESIGN OF LOW ASPECT RATIO WING-WINGLET CONFIGURATIONS FOR TRANSONIC WIND-TUNNEL TESTS Kuhiman, John M. et al. National Aeronautics and Space Administration	7 テクニカルペーパー Low-Speed Wind Tunnel Tests on a Lambda Wing High-Lift Configuration Ghee, T., Taylor, N. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー COMPUTATIONAL DESIGN OF LOW ASPECT RATIO WING-WINCLET CONFIGURATIONS FOR TRANSONIC WIND-TUNNEL TESTS Kuhlman, John M. et al. National Aeronautics and Space Administration	8 テクニカルペーパー Low-Speed Wind Tunnel Tests on a Diamond Wing High-Lift Configuration Ghee,T., Taylor,N. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー THEORETICAL-NUMERICAL STUDY OF FEASIBILITY OF USE OF WINGLETS ON LOW ASPECT RATION WINGS AT SUBSONIC AND TRANSONIC MACH NUMBERS AT REDUCE DRAC Contractor … Kuhiman, John M. et al. National Aeronautics and Space Administration	9 テクニカルペーパー Design and Testing of Low Sonic Boom Configurations and an Oblique All-Wing Supersonic Transport Lee, Christopher A. National Aeronautics and Space Adminstration
4 テクニカルペーパー The Effects of Winglets on Low Aspect Ratio Wings at Supersonic Mach Numbers Keenan, James A., Kuhlman, John M. National Aeronautics and Space Adminstration	10 テクニカルペーパー LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 1: TEST Stewart, V.R. National Aeronautics and Space Administration
5 テクニカルペーパー Effects of Winglets on the Drag of a Low-Aspect-Ratio Configuration Smith, Leigh Ann, Campbell, Richard L. National Aeronautics and Space Adminstration	11 テクニカルペーパー LOW SPEED WIND TUNNEL TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 2: TEST DATA Stewart, V.R. National Aeronautics and Space Administration
6 テクニカルペーパー A Low-Speed Wind Tunnel Study of Vortex Interation Control techniqus on a Chine-Forebody/Delta-Wing Configuration Rao, Dhanvada M., Bhat, M.K. National Aeronautics and Space Adminstration	12 テクニカルペーパー A Review of Standards Model Testing in The Boeing Transonic wind Tunnel (Invited). Belter, D.L., Mejia, K.M., Okada, D.S. American Institute of Aeronautics and Astronautics

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