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

Aerodynamics, Transonic X
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An experimental study of transonic flow about a supercritical airfoil

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983
Format: Print
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Vectorizable multigrid algorithms for transonic flow calculations

Published: [Washington, D.C.? : National Aeronautics and Space Administration, 1985]
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Computation of transonic boattail flow with separation

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1977
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The design of supercritical wings by the use of three-dimensional transonic theory

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, ; 1979
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Numerical study of transonic flow over oscillating airfoils using the full potential equation

Published: Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
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Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
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CAS2D - FORTRAN program for nonrotating blade-to-blade, steady potential transonic cascade flows

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980
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Computation of unsteady transonic flows through rotating and stationary cascades

Published: [Washington] : National Aeronautics and Space Administration, ; Springfield, Va. : for sale by the National Technical Information Service, 1977
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Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row

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
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An experimental investigation of boundary layer and crossflow characteristics of the Ames 2- by 2-foot and 11- by 11-foot transonic wind-tunnel walls

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1977
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Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter 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], 1983
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Further investigation of a finite difference procedure for analyzing the transonic flow about harmonically oscillating airfoils and wings

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980
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Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds

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
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High angle canard missile test in the Ames 11-foot transonic wind tunnel

Published: Washington : National Aeronautics and Space Adiministration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
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High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel

Published: [Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982
Format: Print
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