Blank Cover Image

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

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1989
Issue:
NASA-CR-181939
No.:
G3/02 0252162
Pt.:
NAS 1.26:181939
Paper no.:
N90-17539
Page(from):
1
Page(to):
114
Pages:
114
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper 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 Technical Paper Low-Speed Wind Tunnel Tests on a Lambda Wing High-Lift Configuration

Ghee, T., Taylor, N.

American Institute of Aeronautics and Astronautics
2 Technical Paper 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 Technical Paper Low-Speed Wind Tunnel Tests on a Diamond Wing High-Lift Configuration

Ghee,T., Taylor,N.

American Institute of Aeronautics and Astronautics
3 Technical Paper 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 Technical Paper Design and Testing of Low Sonic Boom Configurations and an Oblique All-Wing Supersonic Transport

Lee, Christopher A.

National Aeronautics and Space Adminstration
4 Technical Paper 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 Technical Paper 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 Technical Paper Effects of Winglets on the Drag of a Low-Aspect-Ratio Configuration

Smith, Leigh Ann, Campbell, Richard L.

National Aeronautics and Space Adminstration
11 Technical Paper 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 Technical Paper 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 Technical Paper 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
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12