The Online Books Page

Books by Harry W. Carlson:

Books in the extended shelves:

• Carlson, Harry W.: Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Christine M. Darden and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Application of sonic-boom minimization concepts in supersonic transport design (National Aeronautics and Space Administration ;, 1973), also by Robert J. Mack, Raymond L. Barger, and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Kenneth B. Walkley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Correlation of sonic-boom theory with wind-tunnel and flight measurements (National Aeronautics and Space Administration, 1964), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust; US access only)
• Carlson, Harry W.: 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 Raymond L. Barger, Robert J. Mack, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Carlson, Harry W.: Estimation of leading-edge thrust for supersonic wings of arbitrary planform (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Robert J. Mack, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert J. Mack, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Carlson, Harry W.: An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations (NACA, 1955), also by John P. Gapcynski, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Carlson, Harry W.: Experimental techniques for predicting store motions during release or ejection (National Advisory Committee for Aeronautics, 1959), also by Maxime A. Faget and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Carlson, Harry W.: An investigation of some aspects of the sonic boom by means of wind-tunnel measurements of pressures about several bodies at a mach number of 2.01 (National Aeronautics and Space Administration :, 1959), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: The lower bound of attainable sonic-boom overpressure and design methods of approaching this limit (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1959), also by Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: A modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Carlson, Harry W.: Numerical methods for the design and analysis of wings at supersonic speeds (National Aeronautics and Space Administration ;, 1974), also by David S. Miller and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Pressure distributions at Mach number 2.05 on a series of highly swept arrow wings employing various degrees of twist and camber (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: Sonic-boom characteristics in the extreme near field of a complex airplane model at mach numbers of 1.5, 1.8, and 2.5 (National Aeronautics and Space Administration, 1970), also by Odell A. Morris, Milton Lamb, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: Sonic-boom characteristics of proposed supersonic and hypersonic airplanes (National Aeronautics and Space Administration, 1966), also by F. Edward McLean, Lynn W. Hunton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Carlson, Harry W.: A study of the application of heat or force fields to the sonic-boom-minimization problem (National Aeronautics and Space Administration, 1969), also by David S. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Robert J. Mack, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Supersonic wings with significant leading-edge thrust at cruise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by A. Warner Robins, Robert J. Mack, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Carlson, Harry W.: Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Michael J. Mann, Christine M. Darden, and Langley Research Center (page images at HathiTrust)
• Carlson, Harry W.: Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Christine M. Darden and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Carlson, Harry W.: Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63 (National Aeronautics and Space Administration, 1971), also by Davis S. Miller, Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carlson, Harry W.: A wind-tunnel investigation of the effect of body shape on sonic-boom pressure distributions (National Aeronautics and Space Administration, 1965), also by Odell A. Morris, Robert J. Mack, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Carlson, Harry W.: A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Robert J. Mack and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

Find more by Harry W. Carlson at your library, or elsewhere.