Pressure probe and hot-film probe responses to acoustic excitation in mean flow /

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. ...

Measurements of mean static pressure and far-field acoustics of shock-containing supersonic jets /

Norum, Thomas D.
Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

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: ...

A short static-pressure probe design for supersonic flow /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

January 1975

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

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

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...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Measurements of farfield sound generation from a flow-excited cavity /

Block, P. J. W.
Heller, H. (Hanno)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

The wedge hot-film anemometer in supersonic flow /

Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"Langley Research Center."Subject category 71."May 1983"--Cover.Mode of access: Internet

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

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...

Experimental validation of a two-dimensional shear-flow model for determining acoustic impedance /

Parrott, Tony L.
Jones, Michael G. (Michael Glen)
Watson, Willie R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 15).Mo...

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...

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. ...

Measurements of mean static pressure and far-field acoustics of shock-containing supersonic jets /

Norum, Thomas D.
Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

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: ...

A short static-pressure probe design for supersonic flow /

Pinckney, S. Z. (Shimer Zane), 1934-
Langley Research Center.

January 1975

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

Experimental cavity pressure distributions at supersonic speeds /

Stallings, Robert L.
Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."June 1987"--Cover.Includes bibliographical references (p. 9).Mo...

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...

Investigation of a supersonic cruise fighter model flow field /

Reubush, David E.
Bare, E. Ann.
Langley Research Center.

January 1985

Prepared at Langley Research Center."November 1985"--Cover.Includes bibliographical references (p. 8...

Measurements of farfield sound generation from a flow-excited cavity /

Block, P. J. W.
Heller, H. (Hanno)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

The wedge hot-film anemometer in supersonic flow /

Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

"Langley Research Center."Subject category 71."May 1983"--Cover.Mode of access: Internet

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Transition fixing for hypersonic flow /

Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."October 1967"--Cover.Includes bibliographical references (p. 12...

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...

Experimental validation of a two-dimensional shear-flow model for determining acoustic impedance /

Parrott, Tony L.
Jones, Michael G. (Michael Glen)
Watson, Willie R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."May 1987"--Cover.Includes bibliographical references (p. 15).Mo...

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...

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. ...

Measurements of mean static pressure and far-field acoustics of shock-containing supersonic jets /

Norum, Thomas D.
Seiner, John M.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

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

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: ...

Pressure probe and hot-film probe responses to acoustic excitation in mean flow /

Abstract

Extracted data

Pressure probe and hot-film probe responses to acoustic excitation in mean flow /

Abstract

Extracted data

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