COMPUTATIONAL DESIGN OF LOW ASPECT RATIO WING-WINGLET CONFIGURATIONS FOR TRANSONIC WIND-TUNNEL TESTS | 東京工業大学附属図書館文献データベース

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

著者名:: Kuhiman, John M. et al. ( West Virginia Univ. )
掲載資料名:: NASA Technical Reports(N88-)
発行年:: 1988
号:: NASA-CR-183021
通号:: G3/05 0148106
パート:: NAS1.26:183021
ペーパー番号:: N88-24630
開始ページ:: 1
終了ページ:: 64
総ページ数:: 64
出版情報:: National Aeronautics and Space Administration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:	ZA00001424
論文注記:	NAG-1-625

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., Brown, Christopher K. National Aeronautics and Space Adminstration	7 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
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 TEST OF A PROPULSIVE WING/CANARD CONCEPT IN THE STOL CONFIGURATION. VOLUME 1: TEST Stewart, V.R. National Aeronautics and Space Administration
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 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
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 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
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 FORWARD-SWEPT WING CONFIGURATION DESIGNED FOR HIGH MANEUVERABILITY BY USE OF A TRANSONIC COMPUTATIONAL METHOD Mann, M.J. National Aeronautics and Space Administration
6 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	12 テクニカルペーパー The Design and Testing of a Winglet Airfoil for Low-Speed Aircraft M.D.,Maughmer, T.S.,Swan, S.M.,Willits American Institute of Aeronautics and Astronautics

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