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1
Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections /
by Goradia, Suresh H. (Suresh Harkisondas), 1937-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
2
TRANDESNF : a computer program for transonic airfoil design and analysis in nonuniform flow /
by Chang, Jen-Fu
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987

Government Document Book
3
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation /
by Barnwell, Richard W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
4
High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by Johnson, William G. (William Garland), 1944-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Book
5
A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord Fowler flap /
by Seetharam, H. C.
Washington, D.C. : National Aeronautics and Space Administration, 1977

Government Document Book
6
Improved method for prediction of attainable leading-edge thrust /
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1996

Book
7
Analysis of unswept and swept wing chordwise pressure data from an oscillating NACA 0012 airfoil experiment /
by St. Hilaire, A. O.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book
8
Low-speed aerodynamic characteristics of a 17-percent-thick airfoil section designed for general aviation applications /
by McGhee, Robert J.
Washington D.C. : Alexandria, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1973

Government Document Book
9
Aerofoil testing in a self-streamlining flexible walled wind tunnel /
by Lewis, Mark Charles
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988

Government Document Book
10
Transonic airfoil flowfield analysis using Cartesian coordinates /
by Carlson, Leland A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
12
Development of a computer program to obtain ordinates from NACA 6- and 6A-series airfoils /
by Ladson, Charles L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
13
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration /
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document Book
14
An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 /
by Re, Richard J.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Book
15
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane /
by Allison, Dennis O.
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service (NTIS) [distributor], 1995

Government Document Book
16
Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /
by McGhee, Robert J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book
17
Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps /
by Bingham, Gene J.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1974

Government Document Book
18
Section data for thin, highly cambered airfoils in incompressible flow /
by Milgram, Jerome H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1971

Government Document Book
19
Analysis of strong-interaction dynamic stall for laminar flow on airfoils /
by Gibeling, H. J., Shamroth, S. J., Eiseman, P. R.
Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book
20
Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by Johnson, William G. (William Garland), 1944-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Book
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