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1
Inverse boundary-layer theory and comparsion with experiment /
by Carter, James E. (James Edward), 1944-
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978

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Government Document Book
2
An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /
by Holloway, Paul F.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1965

Government Document Book
3
Jet-boundary corrections for lifting rotors centered in rectangular wind tunnels /
by Heyson, Harry H.
Washington, D.C. : Springfield, VA : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960

Book
4
Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations /
by Kuhn, Gary D.
Washington, D.C. : National Aeronautics and Space Administration, 1971

Government Document Book
5
Stability of separating subsonic boundary layers /
by Masad, Jamal A. (Jamal Ahmad), 1960-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1994

Government Document Book
6
Higher-order numerical methods derived from three-point polynomial interpolation /
by Rubin, Stanley G.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Government Document Book
7
Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter Transonic Cryogenic Tunnel /
by Murthy, A. V.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988

Government Document Book
8
Assessment of a transitional boundary layer theory at low hypersonic mach numbers /
by Shamroth, S. J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book
9
Nongrey radiation effects on the boundary layer of an absorbing gas over a flat plate /
by Smith, A. M.
Washington, D.C. : National Aeronautics and Space Administration, 1966

Government Document Book
10
Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream /
by McClinton, Charles R.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
11
Boundary-layer velocity profiles downstream of three-dimensional transition trips on a flat plate at Mach 3 and 4 /
by Peterson, John B.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information], 1969

Government Document Book
12
Long-wavelength asymptotics of unstable crossflow modes, including the effect of surface curvature /
by Choudhari, Meelan, 1963-
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994

Government Document Book
13
Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /
by Pfenninger, W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
14
Comparison of measured and calculated velocity profiles of a laminar incompressible free jet at low Reynolds numbers /
by Greene, George C.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
15
Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction /
by Brown, Ronald D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
16
A Review of flight and wind tunnel measurements of boundary layer pressure fluctuations and induced structural response /
by Bies, David A., 1925-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966

Government Document Book
17
Numerical calculation of boundary-induced interference in slotted or perforated wind tunnels including viscous effects in slots /
by Keller, James D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book
18
An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows /
by Gupta, Roop N.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Book
19
Methods for the prediction of the installation aerodynamics of a propfan at subsonic speeds /
by Chandrasekaran, B., 1942-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985

Government Document Book
20
An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube /
by Weilmuenster, K. James
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
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