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raymond l barger

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Reflector AntennasA simplified approach to axisymmetric dual-reflector antenna designRaymond L. Barger

A simplified approach to axisymmetric dual-reflector antenna design

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Division

Sayfa sayısı yok · 1988

Antennas, Reflector / Reflector Antennas

Nonlinear Differential equationsSome path-following techniques for solution of nonlinear equations and comparison with parametric differentiationRaymond L. Barger

Some path-following techniques for solution of nonlinear equations and comparison with parametric differentiation

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1987

Differential equations, Nonlinear / Nonlinear Differential equations

Computational gridsAutomatic computation of Euler-marching and subsonic grids forwing-fuselage configurationsRaymond L. Barger

Automatic computation of Euler-marching and subsonic grids forwing-fuselage configurations

Raymond L. Barger · National Aeronautics and Space Administration, Langley Research Center

18 sayfa · 1994

Aerodynamics / Computational grids

Shock wavesSonic-boom wave-front shapes and curvatures associated with maneuvering flightRaymond L. Barger

Sonic-boom wave-front shapes and curvatures associated with maneuvering flight

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

27 sayfa · 1979

Mathematical models / Aerodynamics / Sonic boom / Shock waves

Supersonic AerodynamicsInvestigation of flow characteristics over missle bodies at supersonic speedsRaymond L. Barger

Investigation of flow characteristics over missle bodies at supersonic speeds

Raymond L. Barger · For sale by the National Technical Information Service]

38 sayfa · 1979

Aerodynamics, Supersonic / Flow visualization / Guided missiles / Supersonic Aerodynamics

Shock (Mechanics)Weak-wave analysis of shock ineraction with a slipstreamRaymond L. Barger

Weak-wave analysis of shock ineraction with a slipstream

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Division

Sayfa sayısı yok · 1988

Aerodynamics / Shock (Mechanics)

Surfaces, Models ofTrajectory fitting in function space with application to analytic modeling of surfacesRaymond L. Barger

Trajectory fitting in function space with application to analytic modeling of surfaces

Raymond L. Barger · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1992

Models of Surfaces / Numerical grid generation (Numerical analysis) / Surfaces, Models of

Supersonic AerodynamicsAutomatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraintRaymond L. Barger

Automatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraint

Raymond L. Barger · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1993

Aerodynamics, Supersonic / Supersonic Aerodynamics

Acoustical engineeringTheoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tipsRaymond L. Barger

Theoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tips

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Office

16 sayfa · 1980

Testing / Rotors / Propellers / Noise control / Acoustical engineering

PerformanceTheory for computing the size and shape of a region of influence associated with a maneuvering vehicleRaymond L. Barger

Theory for computing the size and shape of a region of influence associated with a maneuvering vehicle

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

19 sayfa · 1980

Airplanes / Data processing / Mathematical models / Performance

Noses (Aircraft)A theoretical investigation of forebody shapes designed for natural laminar boundary-layer flowRaymond L. Barger

A theoretical investigation of forebody shapes designed for natural laminar boundary-layer flow

Raymond L. Barger · for sale by the National Technical Information Service

15 sayfa · 1978

Boundary layer / Laminar flow / Noses (Aircraft)

Electromagnetic wavesTheory for computing the field scattered from a smooth inflected surfaceRaymond L. Barger

Theory for computing the field scattered from a smooth inflected surface

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1987

Electromagnetic waves

WingsAn Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurationsRaymond L. Barger

An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

17 sayfa · 1982

Airplanes / Wings

Acoustic impedanceA theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effectsRaymond L. Barger

A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

19 sayfa · 1981

Testing / Resonance / Wind tunnels / Acoustic impedance

Shock wave interactionWeak-wave analysis of shock interaction with a slipstreamRaymond L. Barger

Weak-wave analysis of shock interaction with a slipstream

Raymond L. Barger · Langley Research Center

17 sayfa · 1988

Slipstreams / Shock wave interaction

Drag (Aerodynamics)A method for designing blended wing-body configurations for low wave dragRaymond L. Barger

A method for designing blended wing-body configurations for low wave drag

Raymond L. Barger · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1992

Supersonic planes / Drag (Aerodynamics)

Surface geometryAutomatic procedures for computing complete configuration geometry from individual component descriptionsRaymond L. Barger

Automatic procedures for computing complete configuration geometry from individual component descriptions

Raymond L. Barger · Langley Research Center

11 sayfa · 1994

Aircraft configurations / Surface geometry

Vortex-motionA distributed vortex method for computing the vortex field of a missileRaymond L. Barger

A distributed vortex method for computing the vortex field of a missile

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Office

16 sayfa · 1978

Guided missiles / Wakes (Aerodynamics) / Vortex-motion

Surface wavesA procedure for computing surface wave trajectories on an inhomogeneous surfaceRaymond L. Barger

A procedure for computing surface wave trajectories on an inhomogeneous surface

Raymond L. Barger · Langley Research Center

11 sayfa · 1989

Nondestructive tests / Surface waves

Surface geometryAutomatic procedures for computing complete configuration geometry for individual component descriptionsRaymond L. Barger

Automatic procedures for computing complete configuration geometry for individual component descriptions

Raymond L. Barger · National Technical Information Service, distributor

Sayfa sayısı yok · 1994

Aircraft configurations / Computational geometry / Computational grids / Grid generation (Mathematics) / Surface geometry

Surfaces, Models ofSemianalytic modeling of aerodynamic shapesRaymond L. Barger

Semianalytic modeling of aerodynamic shapes

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1985

Aerodynamics / Body of revolution / Computer simulation / Models of Surfaces / Surfaces, Models of

Noise reductionFuselage design for a specified Mach-sliced area distributionRaymond L. Barger

Fuselage design for a specified Mach-sliced area distribution

Raymond L. Barger · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division

Sayfa sayısı yok · 1990

Fuselages / Aircraft design / Aircraft configurations / Mach number / Noise reduction

Supersonic AerodynamicsA performance index approach to aerodynamic design with the use of analysis codes onlyRaymond L. Barger

A performance index approach to aerodynamic design with the use of analysis codes only

Raymond L. Barger · National Aeronautics and Space Administration, Scientific and Technical Information Division

Sayfa sayısı yok · 1988

Aerodynamics, Supersonic / Computer programs / Supersonic Aerodynamics

TakeoffA new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplaneRaymond L. Barger

A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane

Raymond L. Barger · For sale by the National Technical Information Service]

21 sayfa · 1980

Jet planes / Noise / Airplanes / Takeoff

AerodynamicsOn minimizing the number of calculations in design-by-analysis codesRaymond L. Barger

On minimizing the number of calculations in design-by-analysis codes

Raymond L. Barger · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1987

Aerodynamics