Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /

Mohn, Larry Wayne.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center.""July 1975."Cover t...

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

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

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

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /

Wolf, Stephen W. D.
Ames Research Center. Fluid Dynamics Research Branch.

January 1990

Includes indexes.Sponsored by the Fluid Dynamics Research Branch, NASA Ames Research Center, under C...

Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures /

Atvars, J.
Lewis Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Lewis Research Center."Cover title.Includes ...

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Study and development of acoustic treatment for jet engine tailpipes /

Nelsen, M. D.
Langley Research Center.
Boeing Company. AVCO Corporation. Systems Division.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Boeing Company for Langley Research Center.N72-10043.Includes bibliographical refere...

Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /

Schilling, Benferd L.
Wright, Ray H.
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

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...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Developmental design, fabrication, and test of acoustic suppressors for fans of high bypass turbofan engines /

Tucker, R. H.
Lewis Research Center.
Boeing Company. Wichita Division.

January 1974

"Prepared by the Boeing Company, Wichita, Kans. ... for Lewis Research Center."Cover title.Bibliogra...

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 ...

Adaptive wall technology for minimization of wall interferences in transonic wind tunnels /

Wolf, Stephen W. D.
Langley Research Center.

January 1988

"November 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-17919."Includes bib...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /

Mohn, Larry Wayne.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center.""July 1975."Cover t...

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

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

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

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /

Wolf, Stephen W. D.
Ames Research Center. Fluid Dynamics Research Branch.

January 1990

Includes indexes.Sponsored by the Fluid Dynamics Research Branch, NASA Ames Research Center, under C...

Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures /

Atvars, J.
Lewis Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Airplane Company ... for Lewis Research Center."Cover title.Includes ...

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Study and development of acoustic treatment for jet engine tailpipes /

Nelsen, M. D.
Langley Research Center.
Boeing Company. AVCO Corporation. Systems Division.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Boeing Company for Langley Research Center.N72-10043.Includes bibliographical refere...

Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /

Schilling, Benferd L.
Wright, Ray H.
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

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...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Developmental design, fabrication, and test of acoustic suppressors for fans of high bypass turbofan engines /

Tucker, R. H.
Lewis Research Center.
Boeing Company. Wichita Division.

January 1974

"Prepared by the Boeing Company, Wichita, Kans. ... for Lewis Research Center."Cover title.Bibliogra...

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 ...

Adaptive wall technology for minimization of wall interferences in transonic wind tunnels /

Wolf, Stephen W. D.
Langley Research Center.

January 1988

"November 1988"--Cover."Prepared for Langley Research Center under Contract NAS1-17919."Includes bib...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 9).Mode of acc...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /

Mohn, Larry Wayne.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center.""July 1975."Cover t...

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

Creel, Theodore R.
Chen, Fang-Jenq.
Beckwith, Ivan E.
Langley Research Center.

January 1985

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

Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /

Abstract

Extracted data

Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /

Abstract

Extracted data

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