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An aerodynamic tradeoff study of the scissor wing configuration

Selberg, Bruce P.
Rolla, Mo. : University of Missouri-Rolla ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

Calculation of vortex-flap aerodynamic characteristics

Lan, C. Edward (Chuan-Tau Edward), 1935-, author.
Lawrence, Kansas : Flight Research Laboratory, Department of Aerospace Engineering, the University of Kansas ; [Washington, D.C.] : [National Aeronautics and Space Administration], 1985. 1985

Damage arresting composites for shaped vehicles phase II final report

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Design verification and fabrication of active control systems for the DAST ARW-2 high aspect ratio w

McGehee, C. R., author.
Wichita, KS : The Boeign Co. ; Hampton. Virginia : National Aeronautics and Space Administration, Langley Research Center, [1986] 1986

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

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts

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

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

High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary l

Berrier, Bobby L.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

Large-scale advanced prop-fan (LAP) blade design

Sullivan, William E.
[Windsor Locks, Conn.?] : Hamilton Standard Division, United Technologies ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984?] 1984

Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds user manu

Chandrasekaran, B., 1942-
Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986] 1986

NASA and general aviation

Ethell, Jeffrey L.
Washington, DC : Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1986. 1986

NASA N+3 subsonic fixed wing silent efficient low-emissions commercial transport (SELECT) vehicle st

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Prediction of forces and moments for flight vehicle control effectors

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

Space shuttle afterbody aerodynamics/plume simulation data summary

Blackwell, Kenneth L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, December 1978. 1978-

Space shuttle phase B wind tunnel model and test information.

Glynn, J. L.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1988] 1988

Space shuttle phase B wind tunnel model and test information.

Glynn, J. L.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1988] 1988

Use of constrained optimization in the conceptual design of a medium-range subsonic transport

Sliwa, Steven M., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-