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Sonic boom

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• Aerodynamic noise
• Aerodynamics, Supersonic
• Shock waves

• Sonic boom -- Abstracts
• Sonic boom -- Atmospheric effects
• Sonic boom -- Bibliography
• Sonic boom -- Computer programs
• Sonic boom -- Computer simulation
• Sonic boom -- Congresses
• Sonic boom -- Environmental aspects
• Sonic boom -- Evaluation
• Sonic boom -- Mathematical models
• Sonic boom -- Measurement
• Sonic boom -- Measurements
• Sonic boom -- Missouri
• Sonic boom -- Periodicals
• Sonic boom -- Physiological effect
• Sonic boom -- Prevention
• Sonic boom -- Psychological aspects
• Sonic boom -- Research
• Sonic boom -- Simulation methods
• Sonic boom -- Testing

• The effects of sonic boom and similar impulsive noise on structures. - (U.S. Environmental Protection Agency], 1971), by United States. National Bureau of Standards and United States Office of Noise Abatement and Control (page images at HathiTrust; US access only)
• Sonic booms in the sea (Naval Ordnance Laboratory, 1971), by Robert J Urick and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Simulated sonic boom as an avalanche trigger (Forest Service, U.S. Dept. of Agriculture, Rocky Mountain Forest and Range Experiment Station, 1972), by M. Martinelli (page images at HathiTrust)
• 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), by Harry W. Carlson, Robert J. Mack, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• 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), by Harry W. Carlson, Robert J. Mack, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A semiempirical method for obtaining fuselage normal areas from fuselage Mach sliced areas (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Robert J. Mack, Kathy E. Needleman, and Langley Research Center (page images at HathiTrust)
• A methodology for designing aircraft to low sonic boom constraints (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Robert J. Mack, Kathy E. Needleman, and Langley Research Center (page images at HathiTrust)
• Near-field sonic-boom pressure signatures for the space shuttle launch and orbiter vehicles at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by George C. Ashby, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by George C. Ashby, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• 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), by Raymond L. Barger, N. Duane Melson, and Langley Research Center (page images at HathiTrust)
• A preliminary study of the awakening and startle effects of simulated sonic booms (National Aeronautics and Space Administration, 1968), by Jerome S. Lukas and karl D. Kryter (page images at HathiTrust; US access only)
• Sonic boom in turbulence (National Aeronautics and Space Administration ;, 1971), by W. A. Horning, United States National Aeronautics and Space Administration, Langley Research Center, and inc EG & G (page images at HathiTrust)
• The development of a sonic boom simulator with detonable gases (National Aeronautics and Space Administration, 1971), by R. T. Strugielski, United States National Aeronautics and Space Administration, Langley Research Center, and General American Research Division (page images at HathiTrust)
• The shock expansion tube and its application as a sonic boom simulator (National Aeronautics and Space Administration, 1968), by Hugo E. Dahlke, Langley Research Center, LTV Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Subjective reactions to sonic boom (National Aeronautics and Space Administration, 1965), by K. S. Pearsons, Karl D. Kryter, Beranek Bolt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Behavior of the sonic boom shock wave near the sonic cutoff altitude (National Aeronautics and Space Administration ;, 1965), by Manfred P. Friedman, David C. Chou, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA CR-1175 (National Aeronautics and Space Administration ;, 1968), by Anthony Craggs and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Prediction of sonic boom from experimental near-field overpressure data (National Aeronautics and Space Administration, 1975), by C. R. Glatt, S. J. Reiners, D. S. Hague, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Correlation of sonic-boom theory with wind-tunnel and flight measurements (National Aeronautics and Space Administration, 1964), by Harry W. Carlson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• Some effects of flight path and atmospheric variations on the boom propagated from a supersonic aircraft (National Aeronautics and Space Administration, 1964), by Raymond L. Barger, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• Minimization of sonic-boom parameters in real and isothermal atmospheres. (National Aeronautics and Space Administration, 1975), by Christine M. Darden (page images at HathiTrust; US access only)
• Sonic booms from aircraft in maneuvers (National Aeronautics and Space Administration, 1964), by Domenic J. Maglieri, Donald L. Lansing, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of measured and calculated sonic-boom ground patterns due to several different aircraft maneuvers (National Aeronautics and Space Administration, 1965), by Donald L. Lansing, Domenic J. Maglieri, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of flow-field development for a series of sonic-boom wind-tunnel models (National Aeronautics and Space Administration ;, 1971), by Harry L. Runyan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• 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), by Odell A. Morris, Harry W. Carlson, Milton Lamb, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5779 (National Aeronautics and Space Administration :, 1970), by Jay C. Hardin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A study of the application of heat or force fields to the sonic-boom-minimization problem (National Aeronautics and Space Administration, 1969), by David S. Miller, Harry W. Carlson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of sonic boom generated by thin, nonlifting, rectangular wings (National Aeronautics and Space Administration ;, 1971), by Sanford S. Davis, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Airplane size and staging effects on SST cruise sonic boom (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by John B. Whitlow (page images at HathiTrust; US access only)
• Some effects of mach number and geometry on sonic boom (National Aeronautics and Space Administration ;, 1967), by R. M. Hicks, Lynn W. Hunton, Joel P. Mendoza, and Ames Research Center (page images at HathiTrust)
• Laboratory investigation of diffraction and reflection of sonic booms by buildings (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by J. D. Brooks, Richard Lee Barger, and William D. Beasley (page images at HathiTrust; US access only)
• NASA TN D-6446 (National Aeronautics and Space Administration :, 1971), by M. Schorling, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3806 (National Aeronautics and Space Administration :, 1967), by William B. Igoe and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experiments on the effects of atmospheric refraction and airplane accelerations on sonic-boom ground-pressure patterns (National Aeronautics and Space Administration, 1966), by Domenic J. Maglieri, Norman J. McLeod, David A. Hilton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Sonic-boom characteristics of proposed supersonic and hypersonic airplanes (National Aeronautics and Space Administration, 1966), by F. Edward McLean, Lynn W. Hunton, Harry W. Carlson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Some nonasymptotic effects on the sonic boom of large airplanes (National Aeronautics and Space Administration, 1965), by F. Edward McLean, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Measurements of the response of two light airplanes to sonic booms (National Aeronautics and Space Administration :, 1963), by Domenic J. Maglieri, Garland J. Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some effects of wing planform on sonic boom (National Aeronautics and Space Administration ;, 1973), by Lynn W. Hunton, Joel P. Mendoza, R. M. Hicks, and Ames Research Center (page images at HathiTrust)
• Application of sonic-boom minimization concepts in supersonic transport design (National Aeronautics and Space Administration ;, 1973), by Harry W. Carlson, Robert J. Mack, Raymond L. Barger, and Langley Research Center (page images at HathiTrust)
• Microbarograph measurements and interpretations of B-58 sonic booms : Project Big Boom (Sandia Corporation ;, 1961), by Jack W. Reed and Sandia Corporation (page images at HathiTrust; US access only)
• Sonic boom theory (Federal Aviation Administration, 1968), by John O. Powers (page images at HathiTrust)
• The supersonic transport : the sonic boom and you (Federal Aviation Administration, Dept. of Transportation, 1967), by John O. Powers, Kenneth Power, and United States Federal Aviation Administration (page images at HathiTrust; US access only)
• Response of structures to aircraft generated shock waves (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Arde Associates, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)

• Aircraft sonic boom : studies on aircraft flight, aircraft design, and measurement : a bibliography with abstracts : search period covered, 1964-March 1977 (U. S. Dept. of Commerce, National Technical Information, 1977), by United States. National Technical Information Service and Gerald H. Adams (page images at HathiTrust)

• Development of sonic-boom signatures in a stratified atmosphere (National Aeronautics and Space Administration, 1968), by Raymond L. Barger, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Design of bodies to produce specified sonic-boom signatures (National Aeronautics and Space Administration, 1968), by Raymond L. Barger, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A summary of results on sonic-boom pressure-signature variations associated with atmospheric conditions (National Aeronautics and Space Administration, 1968), by I. E. Garrick, Domenic J. Maglieri, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

• Aircraft noise and sonic boom; selected references. (Washington, 1969), by United States. Department of Transportation. Library Services Division and Maria R. Haywood (page images at HathiTrust; US access only)
• Aircraft sonic boom : studies on aircraft flight, aircraft design, and measurement : a bibliography with abstracts : search period covered, 1964-March 1977 (U. S. Dept. of Commerce, National Technical Information, 1977), by United States. National Technical Information Service and Gerald H. Adams (page images at HathiTrust)

• Sonic-boom minimization with nose-bluntness relaxation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Christine M. Darden, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Sonic boom propagation in a stratified atmosphere, with computer program (National Aeronautics and Space Administration, 1969), by Wallace D. Hayes, H. E. Kulsrud, Rudolph C. Haefeli, United States National Aeronautics and Space Administration, Langley Research Center, and Inc Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Computer program for the study of atmospheric effects on sonic booms (National Aeronautics and Space Administration, 1965), by Manfred P. Friedman, Massachusetts Institute of Technology, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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