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

Effect of air contamination in a helium tunnel /

Henderson, Arthur, 1922-
Swalley, Frank E. (Frank Edwin), 1936-
Langley Research Center.

Prepared at Langley Research Center."June 1960."Cover title.Includes bibliographical references (p. ...

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel /

Plentovich, Elizabeth B.
Gloss, Blair B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 8...

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...

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

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)....

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:...

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...

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...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

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

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

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...

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...

Investigation of a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Image degradation in Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"November 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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

Effect of air contamination in a helium tunnel /

Henderson, Arthur, 1922-
Swalley, Frank E. (Frank Edwin), 1936-
Langley Research Center.

Prepared at Langley Research Center."June 1960."Cover title.Includes bibliographical references (p. ...

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel /

Plentovich, Elizabeth B.
Gloss, Blair B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 8...

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...

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

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)....

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:...

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...

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...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

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

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

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...

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...

Investigation of a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

The Cryogenic wind-tunnel concept for high Reynolds number testing /

Kilgore, Robert A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 53-55).Mode ...

Image degradation in Langley 0.3-meter transonic cryogenic tunnel /

Snow, W. L.
Goad, William K.
Burner, Alpheus W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"November 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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

Effect of air contamination in a helium tunnel /

Henderson, Arthur, 1922-
Swalley, Frank E. (Frank Edwin), 1936-
Langley Research Center.

Prepared at Langley Research Center."June 1960."Cover title.Includes bibliographical references (p. ...

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel /

Plentovich, Elizabeth B.
Gloss, Blair B.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 8...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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