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1
Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987Format: Government Document Book
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2
Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing
Washington : Springfield, Va. : U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976Format: Government Document Book
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3
An experimental and theoretical investigation of the effect of nonmetric over-the-wing nacelles on wing-body aerodynamics
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1979Format: Government Document Book
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4
Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1987Format: Government Document Book
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5
Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
[Washington, D.C.] : [Springfield,Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1987Format: Government Document Book
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6
Investigation of a supersonic cruise fighter model flow field
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1985Format: Government Document Book
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7
Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane
Washington, D.C. : [Springfield, Va.] : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982Format: Government Document Book
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8
Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1987Format: Government Document Book
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9
Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983Other Authors: “…Reubush, David E.…”
Format: Government Document Book
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10
Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
[Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987Other Authors: “…Reubush, David E.…”
Format: Government Document Book
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11
Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983Other Authors: “…Reubush, David E.…”
Format: Government Document Book
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12
Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Other Authors: “…Reubush, David E.…”
Format: Government Document Book
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13
Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ; [Fo r sale by the National Technical Information Service], 1979Other Authors: “…Reubush, David E.…”
Format: Government Document Book
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14
Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds
[Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987Other Authors:Format: Government Document Book
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15
Effects of afterbody boattail design and empennage arrangement on aeropropulsive characteristics of a twin-engine fighter model at transonic speeds
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Other Authors:Format: Government Document Book
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16
Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Other Authors: “…Reubush, David E.…”
Format: Government Document Book