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  • High-speed research [microform] : 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994 / edited by David A. McCurdy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • High speed civil transport [microform] : sonic boom softening and aerodynamic optimization / Samson Cheung.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas [microform] / Robert J. Mack, Kathy E. Needleman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
    • 1990

  • 1989 high-speed civil transport studies [microform] / HSCT Concept Development Group, Advanced Commercial Programs, Douglas Aircraft Company.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA [microform] / M. Jahed Djomehri, Larry L. Erickson.

    • Text
    • Moffett Field, Calif. : Ames Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • High-Speed Research, Sonic Boom [microform] : proceedings of a conference .... held at Langley Research Center, Hampton, Virginia, February 25-27, 1992 / compiled by Christine M. Darden.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1992- ]
    • 1992-present

  • Floating shock fitting via lagrangian adaptive meshes [microform] / John Van Rosendale.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • High-speed research [microform] : 1994 Sonic Boom Workshop : atmospheric propagation and acceptability studies / edited by David A. McCurdy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1994]
    • 1994

  • High-speed research, sonic boom [microform] : proceedings of a conference sponsored by the National Aeronautics and Space Administraiton, Washingotn, D.C. and held at Ames Research Center, Moffett Field, California, May 12-14, 1993 / edited by Thomas A. Edwards.

    • Text
    • 1994-present

  • Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport [microform] / Christopher A. Lee.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Supersonic civil airplane study and design [microform] : performance and sonic boom / Samson Cheung.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An edge-based solution-adaptive method applied to the AIRPLANE code [microform] / Rupak Biswas, Scott D. Thomas, Susan E. Cliff.

    • Text
    • [Moffett Field, CA] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Development of multiobjective optimization techniques for sonic boom minimization [microform] / Aditi Chattopadhyay, Johnny R. Narayan, Narayanan Pagaldipti.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Ground-based sensors for the SR-71 sonic boom propagation experiment [microform] / Stephen R. Norris, Edward A. Haering, Jr., and James E. Murray.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Linthicum Heights, MD : Available from the NASA Center for AeroSpace Information ; Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Preliminary airborne measurements for the SR-71 sonic boom propagation experiment [microform] / Edward A. Haering, L.J. Ehernberger, and Stephen A. Whitmore.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Ground-recorded sonic boom signatures of F-18 aircraft in formation flight [microform] / Catherine M. Bahm and Edward A. Haering, Jr.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Enhanced multiobjective optimization technique for comprehensive aerospace design [microform] : final report on NCC2-5150 / by Aditi Chattopadhyay and John N. Rajadas.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Reactions of residents to long-term sonic boom noise environments [microform] / James M. Fields.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Comparisons of methods for predicting community annoyance due to sonic booms [microform] / Harvey H. Hubbard, Kevin P. Shepherd.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Sonic boom propagation codes validated by flight test [microform] / Hugh W. Poling.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Development of multiobjective optimization techniques for sonic boom minimization [microform] : final report on NASA Ames grant no. NCC2-5064, performance period--5/16/94-9/15/96 / principal investigators: Aditi Chattopadhyay and John Narayan Rajadas, Narayanan S. Pagaldipti.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • A methodology for designing aircraft to low sonic boom constraints [microform] / Robert J. Mack, Kathy E. Meedleman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60320

  • Summary of sonic boom rise times observed during FAA community response studies over a 6-month period in the Oklahoma City area [microform] / Domenic J. Maglieri and Victor E. Sothcott.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65342

  • Status and capabilities of sonic boom simulators [microform] / Kevin P. Shepherd, Clemans A. Powell.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85536

  • A study in a new test facility on indoor annoyance caused by sonic booms / Jonathan Rathsam, Alexandra Loubeau, and Jacob Klos.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27807

  • Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model / Raymond Castner, Troy Lake.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30596

  • Exhaust nozzle plume effects on sonic boom test results for vectored nozzles / Raymond Castner.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28438

  • Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49555

  • Experimental measurements of sonic boom signatures using a continuous data acquisition technique / Floyd J. Wilcox, Jr., and Alaa A. Elmiligui.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49559

  • Exhaust nozzle plume and shock wave interaction / Raymond S. Castner, Alaa Elmiligui, Susan Cliff.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51485

  • Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / Raymond Castner [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53006

  • Experimental and computational sonic boom assessment of Boeing N+2 low boom models / Donald A. Durston [and five others].

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57237

  • Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models / Susan E. Cliff [and four others].

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, January 2015.
    • 2015-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo60802

  • Advanced concept studies for supersonic commercial transports entering service in the 2018-2020 period, phase 2 / John Morgenstern [and nineteen others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo61953

  • Lateral cutoff analysis and results from NASA's Farfield Investigation of No-Boom Thresholds / Larry J. Cliatt II [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Armstrong Flight Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68489

  • A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 / George C. Ashby, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71442

  • Comparisons of methods for predicting community annoyance due to sonic booms / Harvey H. Hubbard, Kevin P. Shepherd.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67210

  • Recommendations for using noise monitors to estimate noise exposure during X-59 community tests / Jacob Klos.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2020.
    • 2020-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo150503

  • Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / Floyd J. Wilcox, Jr. [and five others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32718

  • Pilot test of a novel method for assessing community response to low-amplitude sonic booms / Sanford Fidell, Richard D. Horonjeff, Michael Harris.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33322

  • Flight test results on the stability and control of the F-15 Quiet Spike aircraft / Cheng M. Moua [and three others].

    • Text
    • Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32721

  • Waveforms and sonic boom perception and response (WSPR) : low-boom community response program pilot test design, execution, and analysis / Juliet A. Page [and eleven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53498

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