Basic experimental study of the coupling between flow instabilities and incident sound /

Effect of low-frequency tones and turbulent-boundary-layer noise on annoyance /

Shepherd, Kevin P.
Clevenson, Sherman A.
Leatherwood, Jack D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"September 1983"--Cover.Subject category 53.Distributed to depository libraries in microfiche.Includ...

A theoretical and experimental study of hypersonic flow over flared bodies at incidence /

Rakich, John V.
Menees, Gene P.
Ames Research Center.

Prepared at Ames Research Center."January 1966"--Cover.Includes bibliographical references (p. 29-30...

Investigation of jet-installation noise sources under static conditions /

Shearin, John G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 71."August 1983"--Cover.Distributed to depository libraries in microfiche.Includes ...

Fluid shielding of high-velocity jet noise /

Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."January 1984"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data /

Weilmuenster, K. James.
Hamilton, H. Harris.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

An experimental investigation of the velocity fluctuations behind oscillating vanes /

Buell, Donald A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Vortex generation and velocity fluctuations behind oscillating vanes.Prepared at Ames Research Cente...

Experimental study of the thermal-acoustic efficiency in a long turbulent diffusion-flame burner /

Mahan, J. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Lewis Research Center.

January 1983

STAR category 71."August 1983"--Cover.Distributed to depository libraries in microfiche."Virginia Po...

The disturbance flow field produced by an evolving vortex /

Gatski, T. B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Simplified combustion noise theory yielding a prediction of fluctuating pressure level /

Huff, Ronald G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental investigation of tangential blowing applied to a subsonic V/STOL inlet /

Burley, Richard R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 02."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

An initial experimental study of the effect of variations in frequency and impulse on the reduction in temperature recovery factor afforded by large-scale unsteady flow /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"January 22, 1958."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of light source and scattering medium related to vapor-screen flow visualization in a supersonic wind tunnel /

Snow, W. L.
Morris, Odell A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 35."December 1984"--Cover.Distributed to depository libraries in microfiche.Bibliog...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight /

Janardan, B. A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
General Electric Company.

January 1984

"November 1984"--Cover.STAR category 71.Distributed to depository libraries in microfiche."General E...

Analysis of noise measured from a propeller in a wake /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."November 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Effect of low-frequency tones and turbulent-boundary-layer noise on annoyance /

Shepherd, Kevin P.
Clevenson, Sherman A.
Leatherwood, Jack D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"September 1983"--Cover.Subject category 53.Distributed to depository libraries in microfiche.Includ...

A theoretical and experimental study of hypersonic flow over flared bodies at incidence /

Rakich, John V.
Menees, Gene P.
Ames Research Center.

Prepared at Ames Research Center."January 1966"--Cover.Includes bibliographical references (p. 29-30...

Investigation of jet-installation noise sources under static conditions /

Shearin, John G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 71."August 1983"--Cover.Distributed to depository libraries in microfiche.Includes ...

Fluid shielding of high-velocity jet noise /

Goodykoontz, Jack H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."January 1984"--Cover.Distributed to depository libraries in microfiche.Includes bi...

Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data /

Weilmuenster, K. James.
Hamilton, H. Harris.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Distributed to depository libraries in microfiche."May 1983"--Cover.Includes bibliographical referen...

An experimental investigation of the velocity fluctuations behind oscillating vanes /

Buell, Donald A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Vortex generation and velocity fluctuations behind oscillating vanes.Prepared at Ames Research Cente...

Experimental study of the thermal-acoustic efficiency in a long turbulent diffusion-flame burner /

Mahan, J. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Virginia Polytechnic Institute and State University.
Lewis Research Center.

January 1983

STAR category 71."August 1983"--Cover.Distributed to depository libraries in microfiche."Virginia Po...

The disturbance flow field produced by an evolving vortex /

Gatski, T. B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."December 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Simplified combustion noise theory yielding a prediction of fluctuating pressure level /

Huff, Ronald G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 71."February 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental investigation of tangential blowing applied to a subsonic V/STOL inlet /

Burley, Richard R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 02."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes bibl...

An initial experimental study of the effect of variations in frequency and impulse on the reduction in temperature recovery factor afforded by large-scale unsteady flow /

Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"January 22, 1958."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of light source and scattering medium related to vapor-screen flow visualization in a supersonic wind tunnel /

Snow, W. L.
Morris, Odell A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 35."December 1984"--Cover.Distributed to depository libraries in microfiche.Bibliog...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight /

Janardan, B. A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
General Electric Company.

January 1984

"November 1984"--Cover.STAR category 71.Distributed to depository libraries in microfiche."General E...

Analysis of noise measured from a propeller in a wake /

Block, P. J. W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."November 1984"--Cover.Distributed to depository libraries in microfiche.Include...

Effect of low-frequency tones and turbulent-boundary-layer noise on annoyance /

Shepherd, Kevin P.
Clevenson, Sherman A.
Leatherwood, Jack D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"September 1983"--Cover.Subject category 53.Distributed to depository libraries in microfiche.Includ...

A theoretical and experimental study of hypersonic flow over flared bodies at incidence /

Rakich, John V.
Menees, Gene P.
Ames Research Center.

Prepared at Ames Research Center."January 1966"--Cover.Includes bibliographical references (p. 29-30...

Investigation of jet-installation noise sources under static conditions /

Shearin, John G.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 71."August 1983"--Cover.Distributed to depository libraries in microfiche.Includes ...

Basic experimental study of the coupling between flow instabilities and incident sound /

Abstract

Extracted data

Basic experimental study of the coupling between flow instabilities and incident sound /

Abstract

Extracted data

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