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Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from mode

Noonan, Kevin W., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. 1980-

Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard regio

Noonan, Kevin W.
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

Aerodynamic design via control theory

Jameson, Antony, 1934-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988] 1988

Autonomous momentum management for space station final report, 15 October 1984

Huntsville, Ala. : George C. Marshall Space Flight Center, [1984] 1984

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) con

Kemmerly, Guy 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

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds

Carlson, Harry W., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

Evaluation of propfan propulsion applied to general aviation

Awker, R. W.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985] 1985

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-

An experimental investigation of the ground vortex created by a moving jet

Stewart, V. R.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and contr

Hahne, David E. (David Edgar)
[Washington, D.C. : National Aeronautics and Space Administration, 1985] 1985

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) a

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001] 2001

Fourier functional analysis for unsteady aerodynamic modeling

Chin, Suei.
Lawrence, Kan. : Flight Research Laboratory, University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1991

Influence of lift offset on rotorcraft performance

Johnson, Wayne, 1946-
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [2009] 2009

Investigation of active flow control to improve aerodynamic performance of oscillating wings

Narducci, Robert P., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014. 2014-

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 de

Prabhu, Ramadas K.
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001] 2001

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984

Parzych, David J.
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985] 1985

Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fl

Runyan, L. James, author.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1992. 1992-

Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurati

Gatlin, Gregory M. (Gregory Michael)
[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], 1989. 1989

Missile aerodynamics for ascent and re-entry

Watts, G. L., author.
Huntsville, Alabama : National Aeronautics and Space Administration, Langley Research Center, 2012. 2012

Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexa

Balakrishna, S., 1931-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992] 1992

Modeling of longitudinal unsteady aerodynamics of a wing-tail combination

Klein, Vladislav.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999] 1999

Multifidelity analysis and optimization for supersonic design

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center , [2010] 2010

Optimal trajectories for an aerospace plane

Miele, Angelo.
Houston, Tex. : Rice University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990] 1990

Predicted turbine heat transfer for a range of test conditions

Boyle, Robert J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996. 1996-

Prediction of forces and moments for flight vehicle control effectors

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

Preliminary aerodynamic investigation of fan rotor blade morphing

Tweedt, Daniel L. (Daniel Lawrence), author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012. 2012

Pseudosteady-state analysis of nonlinear aircraft maneuvers

Young, John W. (John Worth), 1934- author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Semi-annual status report on NASA grant NAG 1-1087 "identification of aerodynamic models for maneuve

Chin, Suei.
Lawrence, Kan. : Flight Research Laboratory, The University of Kansas Center for Research, Inc., [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-

Synthesis from design requirements of a hybrid system for transport aircraft longitudinal control

Hynes, Charles S., author.
Moffett Field, Calif. : National Aeronautics and, Space Administration, Ames Research Center, [2007] 2007

Technology assessment for large vertical-lift transport tiltrotors

Germanowski, Peter J.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [2010] 2010

Transatmospheric vehicle research final technical report, for the program period December 1, 1985 -

Adelman, Henry G.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free

Ghaffari, Farhad.
Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

Wind tunnel interference effects on tiltrotor testing using computational fluid dynamics

Koning, Witold J. F., author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, March 2016. 2016-

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

Yip, Long P.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985. 1985