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Application of laminar flow control to supersonic transport configurations

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

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

Feasibility and benefits of laminar flow control on supersonic cruise airplanes

Powell, A. G.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

On the instability of hypersonic flow past a flat plate

Blackaby, Nicholas D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Wave phenomena in a high Reynolds number compressible boundary layer

Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1985] 1985

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hol

Stallings, Robert L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-