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Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric anal

Hamilton, H. Harris, author.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980. 1980-

Effect of suction on controlling the secondary instability of boundary layers

El-Hady, Nabil M.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Effects of forebody geometry on subsonic boundary-layer stability

Dodbele, S. S.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990. 1990

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

Applin, Zachary T.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

Hahne, David E. (David Edgar)
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991. 1991

Inverse boundary-layer theory and comparison with experiment

Carter, James E. (James Edward), 1944- author.
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978. 1978

Simulated-airline-service flight tests of laminar flow control with perforated-surface suction syste

Maddalon, Dal V., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, March 1990. 1990-

Structural tests and development of a laminar flow control wing surface composite chordwise joint

Lineberger, L. B.
Marietta, Ga. : Lockheed-Georgia Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984] 1984