Raymond L. Barger

Books by Raymond L. Barger

Total count: 37

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

  National Aeronautics and Space Administration, Scientific and Technical Information Office1978-01-01
• A theoretical investigation of forebody shapes designed for natural laminar boundary-layer flow

  for sale by the National Technical Information Service1978-01-01
• Investigation of flow characteristics over missle bodies at supersonic speeds

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1979-01-01
• Sonic-boom wave-front shapes and curvatures associated with maneuvering flight

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1979-01-01
• Sonic-boom wave-front shapes and curvatures associated with maneuvering flight

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1979-01-01
• Investigation of flow characteristics over missle bodies at supersonic speeds

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1979-01-01
• Sonic-boom wave-front shapes and curvatures associated with maneuvering flight

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1979-01-01
• Theoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tips

  National Aeronautics and Space Administration, Scientific and Technical Information Office1980-01-01
• A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane

  For sale by the National Technical Information Service]1980-01-01
• Theory for computing the size and shape of a region of influence associated with a maneuvering vehicle

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1980-01-01
• Theoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tips

  For sale by the National Technical Information Service1980-01-01
• Theory for computing the size and shape of a region of influence associated with a maneuvering vehicle

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1980-01-01
• A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1981-01-01
• A procedure for designing forebodies with constraints on cross-section shape and axial area distribution

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1981-01-01
• Solution of complex nonlinear problems by a generalized application of the method of base and comparison solutions with applications to aerodynamics problems

  For sale by the National Technical Information Service]1981-01-01
• A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1981-01-01
• An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1982-01-01
• An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations

  For sale by the National Technical Information Service]1982-01-01
• Semianalytic modeling of aerodynamic shapes

  National Aeronautics and Space Administration, Scientific and Technical Information Branch1985-01-01
• Theory for computing the field scattered from a smooth inflected surface

  Langley Research Center1986-01-01
and 17 more