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Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaus

[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002] 2002

Acoustic and laser doppler anemometer results for confluent and 12-lobed Ep3s mixer exhaust systems

[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002] 2002

Acoustically tailored composite rotorcraft fuselage panels

Hambric, Stephen A., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015. 2015-

Aerodynamic design and computational analysis of a spacecraft cabin ventilation fan

Tweedt, Daniel L. (Daniel Lawrence)
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Comparison of speech intelligibility in cockpit noise using SPH-4 flight helmet with and without act

Chan, Jeffrey W.
Menlo Park, Calif. : DEV AIR Technical Associates ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Computational aerodynamic simulations of a spacecraft cabin ventilation fan design

Tweedt, Daniel L. (Daniel Lawrence)
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Data quality analysis at the National Transonic Facility

Stewart, Pamela N.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, [1990] 1990

Development of rotorcraft interior noise control concepts phase III, development of noise control co

Yoerkie, C. A., author.
Stratford, CT United Technologies Corporation, Sikorsky Aircraft Division ; Cambridge, MA : Cambrldge Collaborative, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987] 1987

Distribution system simulator

Bahrami, K. A.
Pasadena, Calif. : Jet Propulsion Laboratory, California Institute of Technology, [1986] 1986

Experimental measurement of structural power flow on an aircraft fuselage progress report no. 6, Jan

Cuschieri, J. M. (Joseph M.)
Boca Rotan, Fla. : Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

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 acoustic measurements on a light twin-engined turboprop airplane

Wilby, John F.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Jet shielding of jet noise

Simonich, John C. (John Charles), author.
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986. 1986

Low-speed wind tunnel investigation of the static stability and control characteristics of an advanc

Rhodes, Graham Scott.
Raleigh, N.C. : North Carolina State University ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center], 1990. 1990

A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by

Barger, Raymond L., author.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. 1980-

Phase averaged measurements of the coherent structure of a Mach number 0.6 jet

Emami, Saied, author.
[College Station, TX] : Texas A&M University ; [Washington D.C. : National Aeronautics and Space Administration], December 1983. 1983-

Quadratic optimization in the problems of active control of sound

Loncaric, J. (Josip)
Hampton, Va. : ICASE, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 2002] 2002

Rotorcraft transmission noise path model, including distributed fluid film bearing impedance modelin

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

A simulator study for the development and evaluation of operating procedures on a supersonic cruise

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

Study of noise transmission through double wall aircraft windows

Vaicaitis, R.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983] 1983

Turbofan aft duct suppressor study

Syed, A. A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1983] 1983

Turbofan aft duct suppressor study contractor's data report of mode probe signal data

[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1983?] 1983