Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor /

The wind-induced loads on a dynamically scaled model of a large missile in launching position /

Buell, Donald A.
Kenyon, George C.
Ames Research Center.

January 1959

"December 1959."Caption title.Includes bibliographical refereneces (p. 13).Mode of access: Internet

Steady-state electrical performance of a 400-Hertz Brayton cycle turboalternator and controls /

Valgora, Martin E.
Perz, Dennis A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1970."Cover title.Includes bibliographical references (p...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

A comparison of the performance of four side-mounted inlets over a Mach number range of 0.88 to 2.2 and angles of attack to 14° /

Presley, Leroy L.
Peterson, William P.
Ames Research Center.

January 1960

"January 1960."Caption title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Effect of high rotor pressure-surface diffusion on performance of a transonic turbine /

Miser, James W.
Monroe, Daniel E.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"November 3, 1955."Includes bibliographical references (p. 14-15).Mode of access: Internet

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /

Driver, Cornelius.
Langley Research Center.

January 1959

"September 1959."Caption title.Includes bibliographical references (p. 6).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Performance of a composite solid propellant at simulated high altitudes /

Ciepluch, Carl C.
Langley Research Center.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 /

Norton, Harry T.
Mercer, Charles E.
Cassetti, Marlowe D.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

The wind-induced loads on a dynamically scaled model of a large missile in launching position /

Buell, Donald A.
Kenyon, George C.
Ames Research Center.

January 1959

"December 1959."Caption title.Includes bibliographical refereneces (p. 13).Mode of access: Internet

Steady-state electrical performance of a 400-Hertz Brayton cycle turboalternator and controls /

Valgora, Martin E.
Perz, Dennis A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1970."Cover title.Includes bibliographical references (p...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Effect of a reduction in stator solidity on performance of a transonic turbine /

Miser, James W.
Wong, Robert Y.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

Critical-speed analysis of flexibly mounted rigid rotors /

Cavicchi, Richard H.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 50).Mode of access: Internet

A comparison of the performance of four side-mounted inlets over a Mach number range of 0.88 to 2.2 and angles of attack to 14° /

Presley, Leroy L.
Peterson, William P.
Ames Research Center.

January 1960

"January 1960."Caption title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Effect of high rotor pressure-surface diffusion on performance of a transonic turbine /

Miser, James W.
Monroe, Daniel E.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"November 3, 1955."Includes bibliographical references (p. 14-15).Mode of access: Internet

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /

Driver, Cornelius.
Langley Research Center.

January 1959

"September 1959."Caption title.Includes bibliographical references (p. 6).Mode of access: Internet

Pressure measurements on a hypersonic glide configuration having 79.5° sweepback and 45° dihedral at a Mach number of 4.95 /

Cooper, Morton.
Gunn, Charles R.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 8).Mode of access: Inte...

Performance of a composite solid propellant at simulated high altitudes /

Ciepluch, Carl C.
Langley Research Center.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle /

Levin, Alan D.
Smith, Ronald C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 18).Mode of access: Internet

Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 /

Norton, Harry T.
Mercer, Charles E.
Cassetti, Marlowe D.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

The wind-induced loads on a dynamically scaled model of a large missile in launching position /

Buell, Donald A.
Kenyon, George C.
Ames Research Center.

January 1959

"December 1959."Caption title.Includes bibliographical refereneces (p. 13).Mode of access: Internet

Steady-state electrical performance of a 400-Hertz Brayton cycle turboalternator and controls /

Valgora, Martin E.
Perz, Dennis A.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Prepared at Lewis Research Center."February 1970."Cover title.Includes bibliographical references (p...

Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."January 1967."Includes bibliographical references.Mode of access: Internet

Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor /

Abstract

Extracted data

Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor /

Abstract

Extracted data

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