1 Result #1: A regression analysis of measured and modeled sonic booms across a lateral microphone array [2025] Added June 2025 Creators & Contributors: Durrant, J. Taggart; Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2025 NAS 1.15:20230001411 Loading... FIND IT Online Connect to online resource Check availability
2 Result #2: Literature review of cumulative noise metrics relevant to X-59 supersonic overflights [2024] Creators & Contributors: Vaughn, Aaron Burton, 1994-; Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2024 NAS 1.15:20240005399 Loading... FIND IT Online Connect to online resource Check availability
3 Result #3: Sonic boom analyses in support of improved X-59 community noise testing [2024] Creators & Contributors: Gee, Kent L.; Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2024 NAS 1.26:20240008985 Loading... FIND IT Online Connect to online resource Check availability
4 Result #4: Recommendations for using noise monitors to estimate noise exposure during X-59 community tests [2020] Creators & Contributors: Klos, Jacob; Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2020 NAS 1.15:20205007926 Loading... FIND IT Online Connect to online resource Check availability
5 Result #5: Sonic booms in atmospheric turbulence (SonicBAT): the influence of turbulence on shaped sonic booms [2020] Creators & Contributors: Bradley, Kevin A.; NASA Neil A. Armstrong Flight Research Center E-Book Edwards, California : National Aeronautics and Space Administration, Armstrong Flight Research Center, [April 2020] NAS 1.26:2020-220509 Loading... FIND IT Online Connect to online resource Check availability
6 Result #6: Field evaluations of sampling, interviewing, and flight tracking of NASA's low boom flight demonstrator aircraft [2019] Creators & Contributors: Fidell, S. A. (Sanford A.); Horonjeff, Richard D. +1 more E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2019 NAS 1.26:2019-220257 Loading... FIND IT Online Connect to online resource Check availability
7 Result #7: Statistical modeling of quiet sonic boom community response survey data [2019] Creators & Contributors: Lee, Jasme; Wilson, Alyson +1 more E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2019 NAS 1.15:2019-220427 Loading... FIND IT Online Connect to online resource Check availability
8 Result #8: Lateral cutoff analysis and results from NASA's Farfield Investigation of No-Boom Thresholds [2016] Creators & Contributors: Cliatt, Larry J.; NASA Neil A. Armstrong Flight Research Center E-Book Edwards, California : National Aeronautics and Space Administration, Armstrong Flight Research Center, February 2016 NAS 1.15:2016-218850 Loading... FIND IT Online Connect to online resource Check availability
9 Result #9: Advanced concept studies for supersonic commercial transports entering service in the 2018-2020 period, phase 2 [2015] Creators & Contributors: Morgenstern, John; NASA Glenn Research Center E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2015 NAS 1.26:2015-218719 Loading... FIND IT Online Connect to online resource Check availability
10 Result #10: Experimental and computational sonic boom assessment of Boeing N+2 low boom models [2015] Creators & Contributors: Durston, D. A.; Ames Research Center E-Book Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, February 2015 NAS 1.60:2015-218482 Loading... FIND IT Online Connect to online resource Check availability
11 Result #11: Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models [2015] Creators & Contributors: Cliff, Susan E.; Ames Research Center E-Book Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, January 2015 NAS 1.60:2015-218483 Loading... FIND IT Online Connect to online resource Check availability
12 Result #12: Waveforms and sonic boom perception and response (WSPR): low-boom community response program pilot test design, execution, and analysis [2014] Creators & Contributors: Page, Juliet A.; Langley Research Center +1 more E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014 NAS 1.26:2014-218180 Loading... FIND IT Online Connect to online resource Check availability
13 Result #13: Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel [2013] Creators & Contributors: Castner, Raymond S.; NASA Glenn Research Center +1 more E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013 NAS 1.15:2013-217903 Loading... FIND IT Online Connect to online resource Check availability
14 Result #14: Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel [2013] Creators & Contributors: Wilcox, Floyd J. (Floyd Jay); Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013 NAS 1.60:2013-218036 Loading... FIND IT Online Connect to online resource Check availability
15 Result #15: Exhaust nozzle plume and shock wave interaction [2013] Creators & Contributors: Castner, Raymond S.; Elmiligui, Alaa +4 more E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013 NAS 1.15:2013-217838 Loading... FIND IT Online Connect to online resource Check availability
16 Result #16: Experimental measurements of sonic boom signatures using a continuous data acquisition technique [2013] Creators & Contributors: Wilcox, Floyd J. (Floyd Jay); Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013 NAS 1.60:2013-218035 Loading... FIND IT Online Connect to online resource Check availability
17 Result #17: Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [2012] Creators & Contributors: Castner, Raymond S.; NASA Glenn Research Center E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] NAS 1.15:2012-217229 Loading... FIND IT Online Connect to online resource Check availability
18 Result #18: Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model [2012] Creators & Contributors: Castner, Raymond; Lake, Troy +1 more E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] NAS 1.15:2012-217446 Loading... FIND IT Online Connect to online resource Check availability
19 Result #19: Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration [2012] Creators & Contributors: Wilcox, Floyd J. (Floyd Jay); Langley Research Center +1 more E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] NAS 1.15:2012-217598 Loading... FIND IT Online Connect to online resource Check availability
20 Result #20: Flight test results on the stability and control of the F-15 Quiet Spike aircraft [2012] Creators & Contributors: Moua, Cheng M.; Hugh L. Dryden Flight Research Center +1 more E-Book Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012] NAS 1.15:2012-215978 Loading... FIND IT Online Connect to online resource Check availability
21 Result #21: Pilot test of a novel method for assessing community response to low-amplitude sonic booms [2012] Creators & Contributors: Fidell, S. A. (Sanford A.); Horonjeff, Richard D. +3 more E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] NAS 1.26:2012-217767 Loading... FIND IT Online Connect to online resource Check availability
22 Result #22: A study in a new test facility on indoor annoyance caused by sonic booms [2012] Creators & Contributors: Rathsam, Jonathan; Loubeau, Alexandra +2 more E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] NAS 1.15:2012-217332 Loading... FIND IT Online Connect to online resource Check availability
23 Result #23: A compilation of Space Shuttle sonic boom measurements [2011] Creators & Contributors: Maglieri, Domenic J.; Langley Research Center E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] NAS 1.26:2011-217080 Loading... FIND IT Online Connect to online resource Check availability
24 Result #24: Computational analysis of a low-boom supersonic inlet [2011] Creators & Contributors: Chima, Rodrick V.; NASA Glenn Research Center E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011] NAS 1.15:2011-217223 Loading... FIND IT Online Connect to online resource Check availability
25 Result #25: Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry [2011] Creators & Contributors: Herring, Gregory C.; Meyers, James F. +1 more E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] NAS 1.15:2011-217052 Loading... FIND IT Online Connect to online resource Check availability
26 Result #26: Equivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations [2011] Creators & Contributors: Tinetti, Ana F.; Langley Research Center E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] NAS 1.26:2011-217078 Loading... FIND IT Online Connect to online resource Check availability
27 Result #27: Focused and steady-state characteristics of shaped sonic boom signatures: prediction and analysis [2011] Creators & Contributors: Maglieri, Domenic J.; Langley Research Center E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] NAS 1.26:2011-217156 Loading... FIND IT Online Connect to online resource Check availability
28 Result #28: Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet [2011] Creators & Contributors: Maglieri, Domenic J.; Henderson, Herbert R. +2 more E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] NAS 1.26:2011-217077 Loading... FIND IT Online Connect to online resource Check availability
29 Result #29: Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [2010] Creators & Contributors: Castner, Raymond S.; NASA Glenn Research Center E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] NAS 1.15:2010-216258 Loading... FIND IT Online Connect to online resource Check availability
30 Result #30: Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles [2010] Creators & Contributors: Castner, Raymond S.; NASA Glenn Research Center E-Book Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] NAS 1.15:2010-216259 Loading... FIND IT Online Connect to online resource Check availability
31 Result #31: CFD analysis of nozzle jet plume effects on sonic boom signature [2009] Creators & Contributors: Bui, Trong T.; NASA Dryden Flight Research Center E-Book Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center, [2009] NAS 1.15:2009-214650 Loading... FIND IT Online Connect to online resource Check availability
32 Result #32: An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts [2005] Creators & Contributors: Mack, Robert J.; Langley Research Center E-Book Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] NAS 1.15:2005-213927 Loading... FIND IT Online Connect to online resource Check availability
33 Result #33: Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [1999] Creators & Contributors: Mack, Robert J.; Langley Research Center E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1999 NAS 1.15:209534 Loading... FIND IT Online Connect to online version Check availability
34 Result #34: Comparisons of methods for predicting community annoyance due to sonic booms [1996] Creators & Contributors: Hubbard, Harvey H.; Shepherd, Kevin P. +1 more E-Book Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996 NAS 1.15:110289 Loading... FIND IT Online Connect to online resource Check availability
35 Result #35: An optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pressure measurements [1996] Creators & Contributors: Whitmore, Stephen A.; Haering, Edward A. +2 more E-Book [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, [1996] NAS 1.60:4000 Loading... FIND IT Online Connect to online resource Check availability
36 Result #36: A methodology for designing aircraft to low sonic boom constraints [1991] Creators & Contributors: Mack, Robert J.; Needleman, Kathy E. +2 more Book (Microfiche) [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991 NAS 1.15:4246 Loading... FIND IT Online Connect to online version (PDF) Check availability
37 Result #37: Summary of sonic boom rise times observed during FAA community response studies over a 6-month period in the Oklahoma City area [1990] Creators & Contributors: Maglieri, Domenic J.; Sothcott, Victor E. +2 more Book (Microfiche) Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 NAS 1.26:4277 Loading... FIND IT Online Connect to online version (PDF) Check availability
38 Result #38: Status and capabilities of sonic boom simulators [1986] Creators & Contributors: Shepherd, Kevin P.; Powell, Clemans A. +1 more Book (Microfiche) Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986] NAS 1.15:87664 Loading... FIND IT Online Connect to online version (PDF) Check availability
39 Result #39: A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 [1980] Creators & Contributors: Ashby, George C.; Langley Research Center +1 more E-Book [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980 NAS 1.60:1787 Loading... FIND IT Online Connect to online resource Check availability
40 Result #40: A nonlinear theory for sonic-boom calculations in a stratified atmosphere [1973] Creators & Contributors: Schorling, M. (Michael); United States National Aeronautics and Space Administration +1 more E-Book Washington, D.C. : National Aeronautics and Space Administration, March 1973 NAS 1.14:D-7105 Loading... FIND IT Online Connect to online resource Check availability
41 Result #41: Aircraft noise and sonic boom: selected references [1969] Creators & Contributors: United States Department of Transportation > Library Services Division; Haywood, Maria R. Book (Print/Paper) Washington, 1969 TD 1.15:2 Loading... Available - Sycamore Check availability
42 Result #42: Airplane size and staging effects on SST cruise sonic boom [1968] Creators & Contributors: Whitlow, John B.; United States National Aeronautics and Space Administration E-Book Washington, D.C. : National Aeronautics and Space Administration, July 1968 NAS 1.14:D-4677 Loading... FIND IT Online Connect to online resource Check availability
43 Result #43: Development of sonic-boom signatures in a stratified atmosphere [1968] Creators & Contributors: Barger, Raymond L.; United States National Aeronautics and Space Administration E-Book Washington, D.C. : National Aeronautics and Space Administration, November 1968 NAS 1.14:D-4890 Loading... FIND IT Online Connect to online resource Check availability
44 Result #44: An estimate of the supersonic flow field about an axisymmetric body with an N wave pressure trace [1968] Creators & Contributors: Luidens, Roger W.; United States National Aeronautics and Space Administration E-Book Washington, D.C. : National Aeronautics and Space Administration, December 1968 NAS 1.14:D-4935 Loading... FIND IT Online Connect to online resource Check availability