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Check calibration of the NASA Glenn 10- by 10-foot supersonic wind tunnel (2014 test entry)

Johnson, Aaron, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2016. 2016-

A data base and analysis program for shuttle main engine dynamic pressure measurements final report

Coffin, Thomas.
[Huntsville, Ala.] : Wyle Laboratories Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986] 1986

Development of optical diaphragm deflection sensors final report

[Alliance, Ohio] : The Babcock & Wilcox Company, Research and Development Division ; Cleveland, Ohio : National Aeronautics and Space Administration, NASA Lewis Research Center, [1985?] 1985

Dimension determination of precursive stall events in a single stage high speed compressor

Bright, Michelle M., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996. 1996-

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-

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle

Brase, L. O.
[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

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-

Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine i

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

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

Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at

Bowman, James S. (James Scarboro), 1924-
[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

Modern experimental techniques in turbine engine testing

Lepicovsky, Jan, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996. 1996-

NACA 0015 wing pressure and trailing vortex measurements

McAlister, Kenneth W.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service , distributor], 1991. 1991

An optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pre

Whitmore, Stephen A.
[Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, [1996] 1996

Stand Alone Pressure Measurement Device (SAPMD) for the space shuttle orbiter final report [pts. 1-

Tomlinson, Bill.
[San Antonio, Tex. : Southwest Research Institute] ; Houston, Tex. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, [1989] 1989

The study of pressure measurement techniques and devices in the range of 10[exp-1] to 10[exp-5] torr

Hoffman, John H.
[Washington, D.C.] : National Aeronautics and Space Administration, [1990] 1990

Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery

King, Paul I.
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfiled, Va. : For sale by the National Technical Information Service, 1991] 1991

A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT fi

[Tullahoma, Tenn. : The University of Tennessee-Calspan Center Aerospace Research (CAR) ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989] 1989