Investigation of the performance of a 78 degree flat-plate helical inducer

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

Cavitation and noncavitation performance of an 80.6 degree flat-plate helical inducer at three rotational speeds / Donald M. Sandercock, Richard F. Soltis and Douglas A. Anderson.

Sandercock, Donald M.
Anderson, Douglas A.
Soltis, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Cavitation performance of an 83° helical inducer operated in liquid hydrogen /

Lewis, George W., Jr.
Sandercock, D. M.
Tysl, Edward R.
Lewis Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 /

Vick, Allen R.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Propulsion system elements.Includes bibliographical references....

An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps /

Montgomery, John C.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsioin system elements; Propulsion systems, liquid-fu...

Evaluation of a hollow, cylindrical, contact-ion source/

Kotnik, J. Thomas
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3.55 /

McDearmon, Russell W.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aircraft; Fluid mechanics.Includes bibliographical references.Mode of a...

Exploratory study of the reduction in friction drag due to streamwise injection of helium.

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Investigation of a 10-centimeter-diameter electron-bombardment ion rocket

Reader, Paul D.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

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

Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine /

Price, Harold G.
Shinn, Arthur M.
Lubick, Robert J.
Lewis Research Center.

January 1962

"July 1962."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

Cavitation and noncavitation performance of an 80.6 degree flat-plate helical inducer at three rotational speeds / Donald M. Sandercock, Richard F. Soltis and Douglas A. Anderson.

Sandercock, Donald M.
Anderson, Douglas A.
Soltis, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Cavitation performance of an 83° helical inducer operated in liquid hydrogen /

Lewis, George W., Jr.
Sandercock, D. M.
Tysl, Edward R.
Lewis Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 /

Vick, Allen R.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Propulsion system elements.Includes bibliographical references....

An experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

Analytical performance characteristics and outlet flow conditions of constant and variable lead helical inducers for cryogenic pumps /

Montgomery, John C.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsioin system elements; Propulsion systems, liquid-fu...

Evaluation of a hollow, cylindrical, contact-ion source/

Kotnik, J. Thomas
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3.55 /

McDearmon, Russell W.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aircraft; Fluid mechanics.Includes bibliographical references.Mode of a...

Exploratory study of the reduction in friction drag due to streamwise injection of helium.

Swenson, Byron L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Investigation of a 10-centimeter-diameter electron-bombardment ion rocket

Reader, Paul D.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

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

Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine /

Price, Harold G.
Shinn, Arthur M.
Lubick, Robert J.
Lewis Research Center.

January 1962

"July 1962."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Induced pressures on cylindrical rods with various nose drags and nose shapes at mach numbers of 17 and 21 /

Witcofski, Robert D.
Henderson, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics.Includes bibliogra...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Cold-air investigation of prototype Snap-8 turbine

Nusbaum, William J.
Holeski, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Fluid mechanics;Power sources, supplementary; Propulsion system elements;...

Investigation of the performance of a 78 degree flat-plate helical inducer

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Investigation of the performance of a 78 degree flat-plate helical inducer

Abstract

Extracted data

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