Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /

Shaw, Robert J.
Neumann, Harvey E., joint author.
Wasserbauer, Joseph F., joint author.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1976

The results of an experimental bleed development study for a full-scale, Mach 2.5, axisymmetric, mix...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 /

Allen, John L.
Mitchell, Glenn A.
Davis, Owen H.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16135.""April 1960"--Cover.Includes bibliographical r...

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Instantaneous distortion in a Mach 2.5, 40-percent-internal-contraction inlet and its effect on turbojet stall margin /

Burstadt, Paul L.
Calogeras, James E.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Digital-computer normal-shock-position and restart control of a Mach 2.5 axisymmetric mixed-compression inlet /

Neiner, George H.
Arpasi, Dale J.
Cole, Gary L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-47.Mode of access: Internet

Throat stability-bypass systems to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction /

Mitchell, Glenn A.
Shaw, Robert J. (Robert Joseph), 1946-
Sanders, Bobby W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ac...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet /

Sanders, Bobby W.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: In...

An experimental investigation at mach numbers from 2.1 to 3.0 of circular internal-compression inlets having translatable centerbodies and provisions for boundary-layer removal /

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

"January 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

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...

Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 /

Davis, Owen H.
Mitchell, Glenn A.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16136.""April 1960"--Cover.Includes bibliographical r...

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /

Shaw, Robert J.
Neumann, Harvey E., joint author.
Wasserbauer, Joseph F., joint author.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1976

The results of an experimental bleed development study for a full-scale, Mach 2.5, axisymmetric, mix...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 /

Allen, John L.
Mitchell, Glenn A.
Davis, Owen H.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16135.""April 1960"--Cover.Includes bibliographical r...

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

Neumann, Harvey E.
Shaw, Robert J. (Robert Joseph), 1946-
Wasserbauer, Joseph F.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design of a bleed system for a Mach 3.5 inlet /

Syberg, J.
Hickcox, T. E.
Ames Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Ames Research Center."Cover title.Bibliography: p. 32.Mode o...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

Instantaneous distortion in a Mach 2.5, 40-percent-internal-contraction inlet and its effect on turbojet stall margin /

Burstadt, Paul L.
Calogeras, James E.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Digital-computer normal-shock-position and restart control of a Mach 2.5 axisymmetric mixed-compression inlet /

Neiner, George H.
Arpasi, Dale J.
Cole, Gary L.
Lewis Research Center.

January 1972

Prepared at Lewis Research Center.Cover title.Bibliography: p. 46-47.Mode of access: Internet

Throat stability-bypass systems to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction /

Mitchell, Glenn A.
Shaw, Robert J. (Robert Joseph), 1946-
Sanders, Bobby W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ac...

Transonic off-design drag and performance of three mixed-compression axisymmetric inlets /

Woollett, Richard R.
Choby, David A.
Meleason, Edward T.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept /

Trexler, Carl A. (Carl Arthur), 1942-
Souders, Sue W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 50).Mode of ...

Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet /

Sanders, Bobby W.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: In...

An experimental investigation at mach numbers from 2.1 to 3.0 of circular internal-compression inlets having translatable centerbodies and provisions for boundary-layer removal /

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

"January 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

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...

Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 /

Davis, Owen H.
Mitchell, Glenn A.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16136.""April 1960"--Cover.Includes bibliographical r...

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /

Shaw, Robert J.
Neumann, Harvey E., joint author.
Wasserbauer, Joseph F., joint author.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1976

The results of an experimental bleed development study for a full-scale, Mach 2.5, axisymmetric, mix...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Performance summary and analysis of a Mach 3.0 design axisymmetric all-external-compression double-cone inlet Mach number range 3.0 to 0.8 /

Allen, John L.
Mitchell, Glenn A.
Davis, Owen H.
Lewis Research Center.

January 1960

"Lewis Research Center, Cleveland, Ohio.""N 63-16135.""April 1960"--Cover.Includes bibliographical r...

Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

Abstract

Extracted data

Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction /

Abstract

Extracted data

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