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

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA (63 sub 1)-012 airfoil

Yu, J. C.

May 1981

The Langley aircraft noise reduction laboratory was used to measure mean flow and turbulence in the ...

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...

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels /

Green, Lawrence L. (Lawrence Lee)
Newman, Perry A.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 18.Mode of access: Internet

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 ...

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 ...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

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...

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 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

Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion /

Booth, Earl R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 7...

Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane /

Underwood, William J.
Abbott, Frank T.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Tests were made at the Langley two-dimensional low-turbulence pressure tunnel of a mode of the NACA ...

Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

Hicks, R. M. (Raymond Morton), 1932-
Bandettini, Angelo.
Mendoza, Joel P.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 8).Mode of acce...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

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.Chiefly graphs.Bibliography: p. 96.Mode of access: Internet

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Apr. 1979."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA (63 sub 1)-012 airfoil

Yu, J. C.

May 1981

The Langley aircraft noise reduction laboratory was used to measure mean flow and turbulence in the ...

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...

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels /

Green, Lawrence L. (Lawrence Lee)
Newman, Perry A.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 18.Mode of access: Internet

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 ...

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 ...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

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...

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 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

Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion /

Booth, Earl R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 7...

Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane /

Underwood, William J.
Abbott, Frank T.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Tests were made at the Langley two-dimensional low-turbulence pressure tunnel of a mode of the NACA ...

Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section /

Hicks, R. M. (Raymond Morton), 1932-
Bandettini, Angelo.
Mendoza, Joel P.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 8).Mode of acce...

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview /

Harris, Charles D., 1952-
Brooks, Cuyler W.
Harvey, William D., 1934-
Langley Research Center.

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 22-24)...

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.Chiefly graphs.Bibliography: p. 96.Mode of access: Internet

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1979

Apr. 1979."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA (63 sub 1)-012 airfoil

Yu, J. C.

May 1981

The Langley aircraft noise reduction laboratory was used to measure mean flow and turbulence in the ...

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...

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels /

Green, Lawrence L. (Lawrence Lee)
Newman, Perry A.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Bibliography: p. 18.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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