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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

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

Interactive calculation procedures for mixed compression inlets

Reshotko, Eli.
Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983] 1983

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

Modelling the transitional boundary layer

Narasimha, R.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

A review of high-speed, convective, heat-transfer computation methods

Tauber, Michael E.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989. 1989