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1
Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air
per Scallion, William I.
Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1999

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2
A comparison of analytical and experimental data for a magnetic actuator
per Groom, Nelson J.
Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2000

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3
Parallel computation with the force /
per Jordan, Harry F. (Harry Frederick)
[Boulder], Colo. : Hampton, Va. : Dept. of Electrical and Computer Engineering ; National Aeronautics and Space Administration, Langley Research Center : Institute for Computer Applications in Science and Engineering, 1985

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4
Shifting the closed-loop spectrum in the optimal linear quadratic regulator problem for hereditary systems : final report /
per Gibson, J. S.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986

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5
Fault-free validation of a fault-tolerant multiprocessor : baseline experiments and workload implementation /
per Feather, Frank
Pittsburgh, Pa. : Hampton, Va. : Carnegie-Mellon University ; National Aeronautics and Space Administration, Langley Research Center, 1986

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6
Noise measurements for a twin-engine commercial jet aircraft during 3 degree approaches and level flyovers /
per Hastings, Earl C.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; for sale by the National Technical Information Service, 1976

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7
On the boundary treatment in spectral methods for hyperbolic systems /
per Canuto, C.
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center : Universities Space Research Association, 1986

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8
Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a mach of 1.41 /
per Dollyhigh, Samuel M.
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; for sale by the National Technical Information Service, 1976

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9
Turbulent-flow separation criteria for overexpanded supersonic nozzles /
per Morrisette, E. Leon
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; for sale by the National Technical Information Service, 1978

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10
Technical update : NESC /

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11
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 200?to 900?/
Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; National Technical Information Service], 1984

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12
NASA Langley scientific and technical information output

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13
Stable boundary conditions and difference schemes for Navier-Stokes equations /
per Dutt, Pravir
Hampton, Va. : Institute for Computer Applications in Science and Engineering, National Aeronautics and Space Administration, Langley Research Center, 1985

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14
Radar cross section studies/compact range research /
per Burnside, W. D. (Walter Dennis), 1942-
Columbus, Ohio : Hampton, Virginia : Ohio State University, ElectroScience Laboratory, Department of Electrical Engineering ; National Aeronautics and Space Administration, Langley Research Center, 1989

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15
On the effect of acoustic coupling on random and harmonic plate vibrations
per Frendi, A.
Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1993

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16
Dynamics of satellite disintegration /
per Dasenbrock, Robert
Washington : Springfield, Va. : Dept. of Defense, Dept. of the Navy, [Office of Naval Research], Naval Research Laboratory ; for sale by the National Technical Information Service, 1976

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17
Method for the prediction of the installation aerodynamics of a propfan at subsonic speeds : user manual /
per Chandrasekaran, B., 1942-
Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, 1986

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18
Three-dimensional transonic potential flow about complex three-dimensional configurations /
per Reyhner, Theodore A.
Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1984

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19
Multigrid solutions to quasi-elliptic schemes /
per Brandt, Achi
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : Institute for Computer Applications in Science and Engineering, 1985

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20
Delamination growth in composite materials /
Newark, Del. : Hampton,Va. : University of Delaware, Center for Composite Materials, College of Engineering ; National Aeronautics and Space Administration, Langley Research Center, 1986

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