Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow /

Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles /

Gertsma, Laurence W.
Yeager, Richard A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Rainey, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications /

Fournier, Roger H.
Langley Research Center.

January 1966

"NASA TM X-1247.""Langley Research Center, Langley Station, Hampton, Va.""August 1966"--Cover.Includ...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

An aerodynamic analysis of Saturn I, Block I flight test vehicles /

Garcia, Fernando S.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."February 1964"--Cover.Includes bibliographical r...

Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/

Hayman, Lovick O.
McDearmon, Russell W.
Langley Research Center.

Prepared at Langley Research Center."March 1962."Cover title.Includes bibliographical references (p....

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel /

Hasel, Lowell E.
Sinclair, Archibald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

January 1950

"April 7, 1950; Declassified May 29, 1959."Includes bibliographical references (p. 14).Mode of acces...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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...

Wind-tunnel investigation of Saturn S-IC AERODYNAMIC engine gimbal forces and base pressures using a cold-flow-jet simulation technique /

Blaha, Bernard J.
Bresnahan, Donald L.
Wasko, Robert A.
Lewis Research Center.

January 1967

"November 1967."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5 /

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 /

Chiccine, Bruce G.
Shinn, Arthur M.
Valerino, Alfred S.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Investigation of a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles /

Gertsma, Laurence W.
Yeager, Richard A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Rainey, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications /

Fournier, Roger H.
Langley Research Center.

January 1966

"NASA TM X-1247.""Langley Research Center, Langley Station, Hampton, Va.""August 1966"--Cover.Includ...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface /

Letko, William.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

An aerodynamic analysis of Saturn I, Block I flight test vehicles /

Garcia, Fernando S.
George C. Marshall Space Flight Center.

Prepared at George C. Marshall Space Flight Center."February 1964"--Cover.Includes bibliographical r...

Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/

Hayman, Lovick O.
McDearmon, Russell W.
Langley Research Center.

Prepared at Langley Research Center."March 1962."Cover title.Includes bibliographical references (p....

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel /

Hasel, Lowell E.
Sinclair, Archibald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

January 1950

"April 7, 1950; Declassified May 29, 1959."Includes bibliographical references (p. 14).Mode of acces...

Supersonic aerodynamics of delta wings /

Wood, Richard M.
Langley Research Center.

January 1988

Prepared at Langley Research Center."March 1988"--Cover.Includes bibliographical references (p. 22-2...

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...

Wind-tunnel investigation of Saturn S-IC AERODYNAMIC engine gimbal forces and base pressures using a cold-flow-jet simulation technique /

Blaha, Bernard J.
Bresnahan, Donald L.
Wasko, Robert A.
Lewis Research Center.

January 1967

"November 1967."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Wind-tunnel investigation of thermal and pressure environments in the base of the Saturn S-IC booster from Mach 0.1 to 3.5 /

Wasko, Robert A.
United States. National Aeronautics and Space Administration.

Cover title."September 1966."Includes bibliographical references.Mode of access: Internet

Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 /

Chiccine, Bruce G.
Shinn, Arthur M.
Valerino, Alfred S.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Investigation of a jet condenser for space power /

Platt, Robert J.
Langley Research Center.

Prepared at Langley Research Center."October 1965"--Cover.Includes bibliographical references (p. 15...

Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles /

Gertsma, Laurence W.
Yeager, Richard A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Rainey, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

Experimental thrust performance of a high-area-ratio rocket nozzle /

Pavli, Albert J.
Smith, Tamara A.
Kacynski, Kenneth J.
Lewis Research Center.

January 1987

Prepared at Lewis Research Center."April 1987"--Cover.Includes bibliographical references (p. 13).Mo...

Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow /

Abstract

Extracted data

Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow /

Abstract

Extracted data

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