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Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement

Glegg, Stewart A. L., author.
London : Academic Press, [2017] 2017

Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading f

Whitney, Warren J., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981. 1981-

Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel

Wilcox, Floyd J., Jr, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013. 2013-

Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speed

Plentovich, Elizabeth B.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991. 1991

Equivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag an

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts

Pittman, Jimmy L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Experimental measurements of sonic boom signatures using a continuous data acquistion technique

Wilcox, Floyd J., Jr, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013. 2013-

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Met

Lawing, Pierce L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate

Parrott, Tony L.
[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], 1989. 1989

Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel

Herring, Gregory C., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2020. 2020-

Fuselage design for a specified Mach-sliced area distribution

Barger, Raymond L.
[Washington, DC] : 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

In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0

Quinn, Robert D., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980. 1980-

Instabilities and subharmonic resonances in subsonic heated round jets

Ng, Lian Lai.
[Tucson, Ariz.] : University of Arizona, Dept. of Aerospace and Mechanical Engineering, 1990. 1990

Investigation of active flow control to improve aerodynamic performance of oscillating wings

Narducci, Robert P., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014. 2014-

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft

Berrier, Bobby L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 de

Prabhu, Ramadas K.
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001] 2001

Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984

Parzych, David J.
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985] 1985

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

Capone, Francis J.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992. 1992

Robust airfoil optimization to achieve consistent drag reduction over a mach range

Li, Wu.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001] 2001