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A distributed vortex method for computing the vortex field of a missile (NASA technical paper) - Raymond L Barger
Theory for computing the size and shape of a region of influence associated with a maneuvering vehicle (NASA technical paper) - Raymond L Barger
An Analytical procedure for computing smooth transitions between two specified cross sections with applications to blended wing-body configurations (N - Raymond L Barger
Automatic computation of Euler-marching and subsonic grids for wing-fuselage configurations (NASA TM) - Raymond L Barger
Investigation of flow characteristics over missle bodies at supersonic speeds (NASA technical paper) - Raymond L Barger
Sonic-boom wave-front shapes and curvatures associated with maneuvering flight (NASA technical paper) - Raymond L Barger
Weak-wave analysis of shock interaction with a slipstream (NASA technical paper) - Raymond L Barger
Solution of complex nonlinear problems by a generalized application of the method of base and comparison solutions with applications to aerodynamics p - Raymond L Barger
On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently (NASA technical note) - Raymond L Barger
A modified Theodorsen [epsilon]-function airfoil design procedure (NASA technical note) - Raymond L Barger
Procedures for the design of low-pitching-moment airfoils (NASA technical note) - Raymond L Barger
Streamline curvature design procedure for subsonic and transonic ducts (NASA technical note) - Raymond L Barger
On minimizing the number of calculations in design-by-analysis codes (NASA technical paper) - Raymond L Barger
A performance index approach to aerodynamic design with the use of analysis codes only (NASA technical paper) - Raymond L Barger
Semianalytic modeling of aerodynamic shapes (NASA technical paper) - Raymond L Barger
A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane (NASA technical paper) - Raymond L Barger
Theoretical prediction of nonlinear propagation effects on noise signatures generated by subconic or supersonic propeller - or rotor-blade tips (NASA - Raymond L Barger