-
1
-
-
0004825913
-
The minimum induced drag of aerofoils
-
Munk, M. M., 'The Minimum Induced Drag of Aerofoils," NACA Report No. 121, 1923.
-
(1923)
NACA Report No. 121
-
-
Munk, M.M.1
-
2
-
-
0242504057
-
The theory of induced lift and minimum induced drag of non-planar lifting systems
-
Cone, C. D., "The Theory of Induced Lift and Minimum Induced Drag of Non-planar Lifting Systems," NACA Technical Report R-139, 1962.
-
(1962)
NACA Technical Report
, vol.R-139
-
-
Cone, C.D.1
-
3
-
-
2942727310
-
A design approach and selected wind tunnel results at high subsonic speeds for wing-tip mounted winglet
-
Whitcomb, R. T., "A Design Approach and Selected Wind Tunnel Results at High Subsonic Speeds for Wing-Tip mounted Winglet", NASA TN-D-8260, 1976.
-
(1976)
NASA TN-D-8260
-
-
Whitcomb, R.T.1
-
5
-
-
84983172654
-
Investigation of aerodynamic improvements using wing tip sails
-
AIAA 99-0530 January 11-14 Reno, Nevada
-
Jarvis, J., and Selberg, B. "Investigation of Aerodynamic Improvements Using Wing Tip Sails", 37th AIAA Aerospace Sciences Meeting, AIAA 99-0530 January 11-14, 1999 Reno, Nevada.
-
(1999)
37th AIAA Aerospace Sciences Meeting
-
-
Jarvis, J.1
Selberg, B.2
-
6
-
-
85081443546
-
Minimum induced drag of wings with winglets
-
September
-
Jones, R., and Lasinski, T. "Minimum Induced Drag of Wings with Winglets" NASA TM-81230, September 1980.
-
(1980)
NASA TM-81230
-
-
Jones, R.1
Lasinski, T.2
-
8
-
-
33845404610
-
An investigation on the effect of raked wing tips
-
Nov.
-
Norton, F.H., "An Investigation on the Effect of Raked Wing Tips", NACA-TN-69, Nov., 1921.
-
(1921)
NACA-TN-69
-
-
Norton, F.H.1
-
9
-
-
0024621548
-
Sheared wing-tip aerodynamics: Wind tunnel and computational investigation
-
March
-
Vijgen, P.M.H.W, Van Dam, C.P., and B. Holmes. "Sheared Wing-Tip Aerodynamics: Wind Tunnel and Computational Investigation." Journal of Aircraft, Vol. 26, No. 3. March 1989.
-
(1989)
Journal of Aircraft
, vol.26
, Issue.3
-
-
Vijgen, P.M.H.W.1
Van Dam, C.P.2
Holmes, B.3
-
10
-
-
0023288642
-
Induced-drag characteristics of crescent-moon-shaped wings
-
Feb
-
VanDam, C. P., "Induced-Drag Characteristics of Crescent-Moon-Shaped Wings", Journal of Aircraft, Vol.24, No.2, Feb 1987.
-
(1987)
Journal of Aircraft
, vol.24
, Issue.2
-
-
VanDam, C.P.1
-
11
-
-
84888834598
-
-
AIAA 90-0300
-
VanDam, C. P., Vijgen, P.M. H. W., Holmes, B. J., "Wind Tunnel Investigation on the Effect of Crescent Planform Shape on Drag, AIAA 90-0300
-
Wind Tunnel Investigation on the Effect of Crescent Planform Shape on Drag
-
-
VanDam, C.P.1
Vijgen, P.M.H.W.2
Holmes, B.J.3
-
14
-
-
85072431721
-
A brief survey of wingtip devices for drag reduction
-
Sept.
-
Rokhsaz, K., "A brief Survey of Wingtip Devices for Drag Reduction," SAE Paper 932574, Sept. 1993.
-
(1993)
SAE Paper 932574
-
-
Rokhsaz, K.1
-
15
-
-
27144467505
-
Biologically inspired fixed-wing configuration studies
-
Sept-Oct
-
Lazos, B. S., "Biologically Inspired Fixed-Wing Configuration Studies," Journal of Aircraft, Vol. 42, No. 5, Sept-Oct, 2005.
-
(2005)
Journal of Aircraft
, vol.42
, Issue.5
-
-
Lazos, B.S.1
-
16
-
-
19644395890
-
The basic aerodynamics research tunnel - A facility dedicated to code validation
-
Sellers, W. L., and Kjelgaard, S. O., "The Basic Aerodynamics Research Tunnel - A Facility Dedicated to Code Validation," AIAA Paper 88-1997, 1988
-
(1988)
AIAA Paper
, vol.88
, Issue.1997
-
-
Sellers, W.L.1
Kjelgaard, S.O.2
-
17
-
-
85081442423
-
-
Selig, M. S., Guglielmo, J. J., Broeren, A. P., and Giguere, P., "Summary of Low-Speed Airfoil Data," Vol. 1, http://www.nasg.com/ardb/ show-polar-e.phtml.
-
Summary of Low-speed Airfoil Data
, vol.1
-
-
Selig, M.S.1
Guglielmo, J.J.2
Broeren, A.P.3
Giguere, P.4
-
18
-
-
0004744139
-
A computational and experimental study of nonlinear aspects of induced drag
-
Feb.
-
Smith, S. C., "A Computational and Experimental Study of Nonlinear Aspects of Induced Drag," NASA Technical Paper No. 3598, Feb. 1996
-
(1996)
NASA Technical Paper No. 3598
-
-
Smith, S.C.1
-
19
-
-
33845440661
-
-
Masters thesis, Royal Institute of Technology (KTH), Sweden, December
-
Melin.T, Tornado, "A vortex lattice MATLAB implementation for Linear Aerodynamic Wing applications", Masters thesis, Royal Institute of Technology (KTH), Sweden, December 2000
-
(2000)
A Vortex Lattice MATLAB Implementation for Linear Aerodynamic Wing Applications
-
-
Tornado, M.T.1
|