Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Directivity and trends of noise generated by a propeller in a wake /

Block, P. J. W.
Gentry, Garl L.
Langley Research Center.

January 1986

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

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /

Berrier, Bobby L.
Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1985

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

Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel /

Beckwith, Ivan E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Keyes, J. Wayne.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 11).Mo...

Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 /

Creel, Theodore R.
Zorumski, W. E.
Beckwith, Ivan E.
Holley, Barbara B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 34."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft /

Mixson, John S.
Roussos, Louis A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 18)....

Effects of propeller rotation direction on airplane interior noise levels /

Willis, Conrad M.
Daniels, Edward F.
Mayes, William H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 5).Mo...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Parametric study of relaminarization of turbulent boundary layers on nozzle walls /

Kreskovsky, J. P.
McDonald, H. (Henry), 1937-
Shamroth, S. J.
Langley Research Center.
United Aircraft Corporation. Research Laboratories.

January 1974

"Prepared by United Aircraft Research Laboratories ... for Langley Research Center."Cover title.Bibl...

Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel /

Molloy, John K.
Keyes, J. Wayne.
Mackley, Ernest A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34243.Includes bibliographical references (p. 30).Mode of a...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Directivity and trends of noise generated by a propeller in a wake /

Block, P. J. W.
Gentry, Garl L.
Langley Research Center.

January 1986

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

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /

Berrier, Bobby L.
Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1985

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

Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel /

Beckwith, Ivan E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 34."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

Modifications to the nozzle test chamber to extend nozzle static-test capability /

Keyes, J. Wayne.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 11).Mo...

Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 /

Creel, Theodore R.
Zorumski, W. E.
Beckwith, Ivan E.
Holley, Barbara B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 34."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

Beckwith, Ivan E.
Holley, Barbara B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

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

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft /

Mixson, John S.
Roussos, Louis A.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 18)....

Effects of propeller rotation direction on airplane interior noise levels /

Willis, Conrad M.
Daniels, Edward F.
Mayes, William H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 5).Mo...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Low-speed wind-tunnel tests of an advanced eight-bladed propeller /

Coe, Paul L.
Dunham, Dana Morris.
Gentry, Garl L.
Langley Research Center.

January 1985

Prepared at Langley Research Center."July 1985"--Cover.Includes bibliographical references (p. 4).Mo...

Parametric study of relaminarization of turbulent boundary layers on nozzle walls /

Kreskovsky, J. P.
McDonald, H. (Henry), 1937-
Shamroth, S. J.
Langley Research Center.
United Aircraft Corporation. Research Laboratories.

January 1974

"Prepared by United Aircraft Research Laboratories ... for Langley Research Center."Cover title.Bibl...

Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel /

Molloy, John K.
Keyes, J. Wayne.
Mackley, Ernest A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34243.Includes bibliographical references (p. 30).Mode of a...

Description and calibration of the Langley hypersonic CF₄ tunnel : a facility for simulating low [gamma] flow as occurs for a real gas /

Midden, Raymond E.
Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1985

Prepared at Langley Research Center."March 1985"--Cover.Includes bibliographical references (p. 16)....

Directivity and trends of noise generated by a propeller in a wake /

Block, P. J. W.
Gentry, Garl L.
Langley Research Center.

January 1986

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

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /

Berrier, Bobby L.
Bangert, Linda S.
Leavitt, Laurence D.
Langley Research Center.

January 1985

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

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Abstract

Extracted data

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel /

Abstract

Extracted data

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