Blank Cover Image

FLIGHT INVESTIGATION OF THE EFFECTS OF AN OUTBOARD WING-LEADING-EDGE MODIFICATION ON STALL/SPIN CHARACTERISTICS OF

Author(s):
Stough, H.P. ( NASA )  
Publication title:
NASA Technical Reports
Pub. Year:
1987
Issue:
NASA-TP-2691
No.:
H1/05 0080033
Pt.:
NAS1.60:2691
Paper no.:
N87-23614
Page(from):
1
Page(to):
117
Pages:
117
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

Similar Items:

1 Technical Paper FLIGHT INVESTIGATION OF THE EFFECT OF TAIL CONFIGURATION ON STALL, SPIN, AND RECOVERY CHARACTERISTICS OF A

Stough, H. P.

National Aeronautics and Space Administration
7 Technical Paper Progress in the Development of Weather Information Systems for the Cockpit.

Stough, H.P., III., Martzaklis, K.S.

Society of Automotive Engineers
2 Technical Paper The Effect of Wing Leading Edge Contamination on the Stall Characteristics of Aircraft.

Tanner, C.E.

Society of Automotive Engineers
8 Technical Paper Flight dynamics and stability and control characteristics of the X-33 vehicle

Lee, H.P., Chang, M., Kaiser, M.K.

American Institute of Aeronautics and Astronautics
3 Technical Paper Numerical Investigation of Reynolds Number Effects on a Blunt Leading-Edge Delta Wing

S. Crippa, A. Rizzi

American Institute of Aeronautics and Astronautics
9 Technical Paper Planform Curvature Effects on Flutter Characteristics of a Wing With 56゜Leading-Edge Sweep and Panel Aspect Ratio of 1.14

Keller, Donald F., Sandford, Maynard C., Pinkerton, Theresa L.

National Aeronautics and Space Adminstration
4 Technical Paper The Effects of Leading Edge Suction on Delta Wing Vortex Breakdown

Maines, B.H., Moeller, B., Rediniotis, O.K.

American Institute of Aeronautics and Astronautics
10 Technical Paper An Experimental Investigation of the Transient Effects Associated with Wing Deployment During Ballistic Flight.

Browning, P., Wilhelm, J.

Society of Automotive Engineers
5 Technical Paper The effects of leading edge suction on delta wing vortex breakdown

Maines, B.H., Moeller, B., Rediniotis, O.K.

American Institute of Aeronautics and Astronautics
11 Technical Paper A LOW SPEED WIND TUNNEL INVESTIGATION OF REYNOLDS NUMBER EFFECTS ON A 60-DEG SWEPT WING CONFIGURATION WITH LEADING AND TRAILING EDGE FLAPS

Rao, Dhanvada M. et al.

National Aeronautics and Space Administration
6 Technical Paper Numerical investigations on the VFE 2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code

A. Schuette, H. Luedeke

American Institute of Aeronautics and Astronautics
12 Technical Paper A Computational Investigation of Dynamic Stall Alleviation using Leading Edge Deformation

Reuster,J., Baeder,J.

American Institute of Aeronautics and Astronautics
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12