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

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

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

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /

Nugent, Jack.
Pendergraft, Odis C.
Ames Research Center.

January 1987

Prepared at Ames Research Center."March 1987"--Cover.Includes bibliographical references (p. 26).Mod...

Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

Johnson, William G. (William Garland), 1944-
Eichmann, Otto.
Hill, Acquilla S.
Langley Research Center.

January 1985

Prepared at Langley Research Center.Bibliography: p. 390.Mode of access: Internet

NACA 0015 wing pressure and trailing vortex measurements /

McAlister, Kenneth W.
Takahashi, R. K.
United States. Army Aeroflightdynamics Directorate.
Ames Research Center.

January 1991

Prepared at Ames Research Center and the U.S. Army Aeroflightdynamics Directorate.Bibliography: p. 2...

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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...

High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds /

Burdges, Kenneth P.
Pounds, Gerald A. (Gerald Autry), 1940-
Blackwell, James A. (James Augusta), 1940-
Langley Research Center.
Lockheed-Georgia Company.

January 1975

Prepared at Lockheed-Georgia Company for Langley Research Center under Contract NAS1-12325.Cover tit...

Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /

Jenkins, Renaldo V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

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...

Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel /

McGhee, Robert J.
Millard, Betty F.
Walker, Betty S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 228).Mode of access: Internet

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil /

Yu, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

Schonester, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

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

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /

Nugent, Jack.
Pendergraft, Odis C.
Ames Research Center.

January 1987

Prepared at Ames Research Center."March 1987"--Cover.Includes bibliographical references (p. 26).Mod...

Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

Johnson, William G. (William Garland), 1944-
Eichmann, Otto.
Hill, Acquilla S.
Langley Research Center.

January 1985

Prepared at Langley Research Center.Bibliography: p. 390.Mode of access: Internet

NACA 0015 wing pressure and trailing vortex measurements /

McAlister, Kenneth W.
Takahashi, R. K.
United States. Army Aeroflightdynamics Directorate.
Ames Research Center.

January 1991

Prepared at Ames Research Center and the U.S. Army Aeroflightdynamics Directorate.Bibliography: p. 2...

Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil /

Beasley, William D.
McGhee, William D.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

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...

High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds /

Burdges, Kenneth P.
Pounds, Gerald A. (Gerald Autry), 1940-
Blackwell, James A. (James Augusta), 1940-
Langley Research Center.
Lockheed-Georgia Company.

January 1975

Prepared at Lockheed-Georgia Company for Langley Research Center under Contract NAS1-12325.Cover tit...

Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /

Jenkins, Renaldo V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

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...

Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel /

McGhee, Robert J.
Millard, Betty F.
Walker, Betty S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 228).Mode of access: Internet

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil /

Yu, James C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

Schonester, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

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

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /

Nugent, Jack.
Pendergraft, Odis C.
Ames Research Center.

January 1987

Prepared at Ames Research Center."March 1987"--Cover.Includes bibliographical references (p. 26).Mod...

Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

Johnson, William G. (William Garland), 1944-
Eichmann, Otto.
Hill, Acquilla S.
Langley Research Center.

January 1985

Prepared at Langley Research Center.Bibliography: p. 390.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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