Study of stator-vane fluctuating pressures in a turbofan engine for static and flight tests /

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

A study of surface pressure fluctuations in hypersonic turbulent boundary layers /

Raman, K. R. (Kizhanatham Raghavachary)
Ames Research Center.
Nielsen Engineering & Research.

"Prepared by Nielsen Engineering & Research ... for Ames Research Center.""February 1974."Cover titl...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

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

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

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...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental determination of the pressure distribution on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30 /

Lessing, Henry C.
Menees, Gene P.
Troutman, John L.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical refe...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

An experimental investigation of the velocity fluctuations behind oscillating vanes /

Buell, Donald A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Vortex generation and velocity fluctuations behind oscillating vanes.Prepared at Ames Research Cente...

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

Nugent, Jack.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer /

Zeydel, E. F. E.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"February, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Int...

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid /

Ashby, George C.
Langley Research Center.

January 1959

"NASA TN D-123.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

A study of surface pressure fluctuations in hypersonic turbulent boundary layers /

Raman, K. R. (Kizhanatham Raghavachary)
Ames Research Center.
Nielsen Engineering & Research.

"Prepared by Nielsen Engineering & Research ... for Ames Research Center.""February 1974."Cover titl...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

Fluctuating pressures on fan blades of a turbofan engine : static and wind-tunnel investigations /

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

January 1982

Subject Category 71."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

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...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Experimental determination of the pressure distribution on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30 /

Lessing, Henry C.
Menees, Gene P.
Troutman, John L.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical refe...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

An experimental investigation of the velocity fluctuations behind oscillating vanes /

Buell, Donald A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Vortex generation and velocity fluctuations behind oscillating vanes.Prepared at Ames Research Cente...

Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter /

Nugent, Jack.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

STAR category 02.Distributed to depository libraries in microfiche."May 1983"--Cover.Includes biblio...

Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer /

Zeydel, E. F. E.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

"February, 1967."Includes bibliographical references."Prepared under contract no.Mode of access: Int...

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Investigation of the effect of a guide-vane-rotor combination on inlet total-pressure distortions in a compressible fluid /

Ashby, George C.
Langley Research Center.

January 1959

"NASA TN D-123.""Langley Research Center, Langley Field, Va.""December 1959."Title from cover.Includ...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

A study of surface pressure fluctuations in hypersonic turbulent boundary layers /

Raman, K. R. (Kizhanatham Raghavachary)
Ames Research Center.
Nielsen Engineering & Research.

"Prepared by Nielsen Engineering & Research ... for Ames Research Center.""February 1974."Cover titl...

Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility /

McDevitt, John B.
Okuno, Arthur F.
Ames Research Center.

January 1985

Prepared at Ames Research Center."June 1985"--Cover.Includes bibliographical references (p. 6).Mode ...

Study of stator-vane fluctuating pressures in a turbofan engine for static and flight tests /

Abstract

Extracted data

Study of stator-vane fluctuating pressures in a turbofan engine for static and flight tests /

Abstract

Extracted data

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