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

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

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

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

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 11...

R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /

Jenkins, Renaldo V.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 9-10)....

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

Hall, R. M.

March 1978

A 0.137m airfoil was tested in a 0.3m transonic cryogenic tunnel at free stream Mach numbers of 0.75...

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel

Hall, R. M.

January 1986

In the context of an overall development of transonic, cryogenic wnd tunnel technology, NASA has bee...

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:...

Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
Langley Research Center.

January 1986

Prepared at Lanagley Research Center."August 1986."Includes bibliographical references (p. 6).Mode o...

Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel /

Poinsatte, Philip E.
Lewis Research Center.
University of Toledo. Dept. of Chemical Engineering.

January 1990

Prepared at the Dept. of Chemical Engineering, University of Toledo, for Lewis Research Center under...

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...

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 ...

A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels /

Adcock, Jerry B.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 09."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel /

Johnson, Charles B.
Stainback, P. Calvin.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 13).Mo...

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel /

Lawing, Pierce L.
Ladson, Charles L.
Adcock, Jerry B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

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

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

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel /

Hall, Robert M.
Langley Research Center.

Prepared at Langley Research Center."January 1986"--Cover.Includes bibliographical references (p. 11...

R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /

Jenkins, Renaldo V.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 9-10)....

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

Hall, R. M.

March 1978

A 0.137m airfoil was tested in a 0.3m transonic cryogenic tunnel at free stream Mach numbers of 0.75...

Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel

Hall, R. M.

January 1986

In the context of an overall development of transonic, cryogenic wnd tunnel technology, NASA has bee...

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:...

Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
Langley Research Center.

January 1986

Prepared at Lanagley Research Center."August 1986."Includes bibliographical references (p. 6).Mode o...

Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel /

Poinsatte, Philip E.
Lewis Research Center.
University of Toledo. Dept. of Chemical Engineering.

January 1990

Prepared at the Dept. of Chemical Engineering, University of Toledo, for Lewis Research Center under...

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...

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 ...

A theoretical analysis of simulated transonic boundary layers in cryogenic-nitrogen wind tunnels /

Adcock, Jerry B.
Johnson, Charles B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 09."March 1980"--Cover."Langley Research Center."Includes bibliographical reference...

Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel /

Johnson, Charles B.
Stainback, P. Calvin.
Langley Research Center.

January 1986

Prepared at Langley Research Center."May 1986"--Cover.Includes bibliographical references (p. 13).Mo...

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel /

Lawing, Pierce L.
Ladson, Charles L.
Adcock, Jerry B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Nov. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

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

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 /

Abstract

Extracted data

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

Abstract

Extracted data

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