Searching Books & More : "United States. National Aeronautics and Space Administration"

Re, Richard J X
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Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
Format: Print
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Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984
Format: Print
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Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984
Format: Print
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An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90

Published: Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1977
Format: Print
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Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979
Format: Print
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Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979
Format: Print
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Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980
Format: Print
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Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982
Format: Print
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Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982
Format: Print
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The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Format: Print
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