Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence /

Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer /

Zeydel, E. F. E.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"February, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Int...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Pilot-aircraft system response to wind shear /

Turkel, Barry S.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS8-33458."Nov. 1980.Includes bibliographical references.Mode of access: Internet

Investigation of refracting flows for acoustic suppression /

Sloan, Denis.
Farquhar, Bannister W., joint author.
Purves, Robert B., joint author.
Boeing Commercial Airplane Company.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Prepared by the Boeing Commercial Airplane Company, under contract no. NAS1-14187, ...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers /

Plentovich, Elizabeth B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 10...

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Technology for pressure-instrumented thin airfoil models /

Wigley, David A.
Langley Research Center.

January 1988

"September 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-18066."Includes bi...

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

Mayer, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

Finite element analysis of aeroacoustic jet-flap flows /

Baker, A. J.
Manhardt, P. D., joint author.
Computational Mechanics Consultants.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1977

Issued Dec. 1977.Prepared for Langley Research Center under Contact NAS 1-14282.Includes bibliograph...

A Review of flight and wind tunnel measurements of boundary layer pressure fluctuations and induced structural response /

Bies, David Alan.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

"October, 1966."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

Bratanow, Theodore.
Kobiske, Michael.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1974

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Acoustic tests of duct-burning turbofan jet noise simulation /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Knott, P. R. (Paul R.)
General Electric Company.
Lewis Research Center.

January 1978

July 1978.Contract NAS 3-18008.Includes bibliographical references.Mode of access: Internet

Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer /

Zeydel, E. F. E.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"February, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Int...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Pilot-aircraft system response to wind shear /

Turkel, Barry S.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS8-33458."Nov. 1980.Includes bibliographical references.Mode of access: Internet

Investigation of refracting flows for acoustic suppression /

Sloan, Denis.
Farquhar, Bannister W., joint author.
Purves, Robert B., joint author.
Boeing Commercial Airplane Company.
United States. National Aeronautics and Space Administration.

January 1977

Issued Apr. 1977.Prepared by the Boeing Commercial Airplane Company, under contract no. NAS1-14187, ...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers /

Plentovich, Elizabeth B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 10...

Aerodynamic and acoustic performance of high Mach number inlets /

Lumsdaine, Edward.
United States. National Aeronautics and Space Administration.

January 1977

Issued Aug. 1977.Includes bibliographical references (p. 12-15).Mode of access: Internet

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Pressure distributions on a 1- by 3-meter semispan wing at sweep angles from 0 ̊to 40 ̊in subsonic flow /

Yip, Long P.
Shubert, l Gary L, joint author.
United States. National Aeronautics and Space Administration.

January 1976

Issued Dec. 1976.Includes bibliographical references (p. 9-10).Mode of access: Internet

Technology for pressure-instrumented thin airfoil models /

Wigley, David A.
Langley Research Center.

January 1988

"September 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-18066."Includes bi...

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

Mayer, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

Finite element analysis of aeroacoustic jet-flap flows /

Baker, A. J.
Manhardt, P. D., joint author.
Computational Mechanics Consultants.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1977

Issued Dec. 1977.Prepared for Langley Research Center under Contact NAS 1-14282.Includes bibliograph...

A Review of flight and wind tunnel measurements of boundary layer pressure fluctuations and induced structural response /

Bies, David Alan.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1966

"October, 1966."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

Numerical calculations of velocity and pressure distribution around oscillating airfoils /

Bratanow, Theodore.
Kobiske, Michael.
Ecer, Akin.
Langley Research Center.
University of Wisconsin--Milwaukee.

January 1974

"Prepared by University of Wisconsin-Milwaukee ... for Langley Research Center."Cover title.Bibliogr...

Acoustic tests of duct-burning turbofan jet noise simulation /

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Knott, P. R. (Paul R.)
General Electric Company.
Lewis Research Center.

January 1978

July 1978.Contract NAS 3-18008.Includes bibliographical references.Mode of access: Internet

Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer /

Zeydel, E. F. E.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"February, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Int...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Pilot-aircraft system response to wind shear /

Turkel, Barry S.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS8-33458."Nov. 1980.Includes bibliographical references.Mode of access: Internet

Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence /

Abstract

Extracted data

Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence /

Abstract

Extracted data

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