The Online Books Page

Online Books by

Raymond L. Barger

Books from the extended shelves:

• Barger, Raymond L.: Adaptation of the Theodorsen theory to the representation of an airfoil as a combination of a lifting line and a thickness distribution (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: 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 Branch ;, 1982), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: Application of sonic-boom minimization concepts in supersonic transport design (National Aeronautics and Space Administration ;, 1973), also by Harry W. Carlson, Robert J. Mack, and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Comparison of jet plume shape predictions and plume influence on sonic boom signature (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by N. Duane Melson and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: The design and operation of a continuous flow electrodeless plasma accelerator (National Aeronautics and Space Administration :, 1962), also by William D. Beasley, Joseph D. Brooks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: Design of bodies to produce specified sonic-boom signatures (National Aeronautics and Space Administration, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: Development of sonic-boom signatures in a stratified atmosphere (National Aeronautics and Space Administration, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: Diffracted and head waves associated with waves on nonseparable surfaces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A distributed vortex method for computing the vortex field of a missile (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Barger, Raymond L.: Estimation of attainable leading-edge thrust for wings at subsonicaand supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Harry W. Carlson, Robert J. Mack, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Barger, Raymond L.: An experimental study of continuous plasma flows driven by a confined arc in a transverse magnetic field (National Aeronautics and Space Administration, 1961), also by William D. Beasley, Joseph D. Brooks, and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Fuselage design for a specified Mach-sliced area distribution (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Mary S. Adams and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Investigation of flow characteristics over missle bodies at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Wallace C. Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: Ionization and deionization processes in low-density plasma flows (National Aeronautics and Space Administration, 1961), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A modified Theodorsen [epsilon]-function airfoil design procedure (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: NASA TN D-5306 (National Aeronautics and Space Administration ;, 1969), also by William D. Beasley, J. D. Brooks, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: A nonlinear theory for airfoils with trailing-edge jet flap (National Aeronautics and Space Administration ;, 1976), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: On minimizing the number of calculations in design-by-analysis codes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Anutosh Moitra and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A performance index approach to aerodynamic design with the use of analysis codes only (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Anutosh Moitra and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A procedure for computing surface wave trajectories on an inhomogeneous surface (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A procedure for designing forebodies with constraints on cross-section shape and axial area distribution (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: Semianalytic modeling of aerodynamic shapes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Mary S. Adams and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A simplified approach to axisymmetric dual-reflector antenna design (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Slender body treatment of some specialized problems associated with elliptic-cross-section missile configurations (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Barger, Raymond L.: Solution of complex nonlinear problems by a generalized application of the method of base and comparison solutions with applications to aerodynamics problems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: Some effects of flight path and atmospheric variations on the boom propagated from a supersonic aircraft (National Aeronautics and Space Administration, 1964), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Some path-following techniques for solution of nonlinear equations and comparison with parametric differentiation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Robert W. Walters and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Sonic-boom wave-front shapes and curvatures associated with maneuvering flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: Streamline curvature design procedure for subsonic and transonic ducts (National Aeronautics and Space Administration ;, 1973), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A streamline curvature method for design of supercritical and subcritical airfoils (National Aeronautics and Space Administration ;, 1974), also by Cuyler W. Brooks and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: A theoretical investigation of forebody shapes designed for natural laminar boundary-layer flow (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Barger, Raymond L.: 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 Office ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Barger, Raymond L.: Theory for computing the field scattered from a smooth inflected surface (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Allen K. Dominek and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: 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 Branch ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Barger, Raymond L.: 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 Branch ;, 1981), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch and Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Trajectory fitting in function space with application to analytic modeling of surfaces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Langley Research Center (page images at HathiTrust)
• Barger, Raymond L.: Weak-wave analysis of shock interaction with a slipstream (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Barger, Raymond L.: Wind-tunnel lift interference on sweptback wings in rectangular test sections with slotted top and bottom walls (National Aeronautics and Space Administration, 1966), also by Ray H. Wright (page images at HathiTrust)

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