Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel /

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) /
by: Arrington, E. Allen
Published: (2012)

Check calibration of the NASA Glenn 10- by 10-foot supersonic wind tunnel (2014 test entry) /
by: Johnson, Aaron, et al.
Published: (2016)

Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet /
by: Maglieri, Domenic J.
Published: (2011)

An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts /
by: Mack, Robert J.
Published: (2005)

Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model /
by: Castner, Raymond
Published: (2012)

Computational analysis of a low-boom supersonic inlet /
by: Chima, Rodrick V.
Published: (2011)

Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel /
by: Pastor-Barsi, Christine, 1982-, et al.
Published: (2018)

Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel /
by: Castner, Raymond S., et al.
Published: (2018)

An experimental device for generating high frequency perturbations in supersonic wind tunnels /
by: Melcher, Kevin J., et al.
Published: (1996)

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by: Mack, Robert J.
Published: (1999)

Sonic boom analyses in support of improved X-59 community noise testing /
by: Gee, Kent L.
Published: (2024)

Exhaust nozzle plume effects on sonic boom test results for vectored nozzles /
by: Castner, Raymond S.
Published: (2012)

A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT : final memorandum report.
Published: (1989)

Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel /
by: Durston, D. A.
Published: (2018)

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
by: Seablom, Kirk D.
Published: (1999)

Experimental measurements of sonic boom signatures using a continuous data acquisition technique /
by: Wilcox, Floyd J. (Floyd Jay)
Published: (2013)

A methodology for designing aircraft to low sonic boom constraints /
by: Mack, Robert J.
Published: (1991)

Contraction design for small low-speed wind tunnels /
by: Bell, J. H.
Published: (1988)

Contraction design for small low-speed wind tunnels /
by: Bell, J. H.
Published: (1988)

Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models /
by: Cliff, Susan E.
Published: (2015)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Focused and steady-state characteristics of shaped sonic boom signatures : prediction and analysis /
Published: (2011)

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /
by: Ashby, George C.
Published: (1980)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

Status and capabilities of sonic boom simulators /
by: Shepherd, Kevin P.
Published: (1986)

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /
by: Hall, Robert M.
Published: (1979)

Slot nozzle effects for reduced sonic boom on a generic supersonic wing section /
by: Castner, Raymond S.
Published: (2010)

CFD analysis of nozzle jet plume effects on sonic boom signature /
by: Bui, Trong T.
Published: (2009)

Uncertainty analysis of the NASA Glenn 8X6 supersonic wind tunnel /
by: Stephens, Julia Elizabeth
Published: (2016)

An optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pressure measurements /
by: Whitmore, Stephen A.
Published: (1996)

An airfoil flutter model suspension system to accommodate large static transonic airloads /
by: Reed, Wilmer H.
Published: (1985)

Flow quality surveys in the settling chamber of the NASA Glenn icing research tunnel (2011 tests) /
by: Steen, Laura E.
Published: (2014)

Analysis of buzz in a supersonic inlet /
by: Chima, Rodrick V.
Published: (2012)