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

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...

Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction

Mitchell, G. A.
Sanders, B. W.
Shaw, R. J.

June 1974

The results of an experimental investigation to increase the stable airflow operating range of a sup...

Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° /

Grimaud, John E.
Langley Research Center.

January 1961

"March 1961."Caption title.Includes bibliographical references (p. 11).Mode of access: Internet

A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet /

Neiner, George H.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Lewis Research Center.""July 1979"-- CoverIncludes bibliographical references.Mode of access: Inter...

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...

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

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

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ac...

Analysis of a stability valve system for extending the dynamic range of a supersonic inlet /

Webb, John A.
Dustin, Miles O.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ac...

Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction /

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

January 1974

The results of an experimental investigation to increase the stable airflow operating range of a sup...

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients /

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...

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...

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...

The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 /

Gawienowski, John J.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Poppet valve control of throat stability bypass to increase stable airflow range of a Mach 2.5. inlet with 60 percent internal contraction /

Mitchell, Glenn A.
Sanders, Bobby W.
Lewis Research Center.

January 1975

The throat of a Mach 2.5 inlet with a coldpipe termination was fitted with a stability-bypass system...

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

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

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...

Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction

Mitchell, G. A.
Sanders, B. W.
Shaw, R. J.

June 1974

The results of an experimental investigation to increase the stable airflow operating range of a sup...

Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° /

Grimaud, John E.
Langley Research Center.

January 1961

"March 1961."Caption title.Includes bibliographical references (p. 11).Mode of access: Internet

A throat-bypass stability-bleed system using relief valves to increase the transient stability of a mixed-compression inlet /

Neiner, George H.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Lewis Research Center.""July 1979"-- CoverIncludes bibliographical references.Mode of access: Inter...

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...

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

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

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 25).Mode of ac...

Analysis of a stability valve system for extending the dynamic range of a supersonic inlet /

Webb, John A.
Dustin, Miles O.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ac...

Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction /

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

January 1974

The results of an experimental investigation to increase the stable airflow operating range of a sup...

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients /

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...

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...

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...

The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3 /

Gawienowski, John J.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Poppet valve control of throat stability bypass to increase stable airflow range of a Mach 2.5. inlet with 60 percent internal contraction /

Mitchell, Glenn A.
Sanders, Bobby W.
Lewis Research Center.

January 1975

The throat of a Mach 2.5 inlet with a coldpipe termination was fitted with a stability-bypass system...

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

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

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...

Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction

Mitchell, G. A.
Sanders, B. W.
Shaw, R. J.

June 1974

The results of an experimental investigation to increase the stable airflow operating range of a sup...

Wind-tunnel investigation at a Mach number of 2.91 of stability and control characteristics of three lifting reentry configurations at angles of attack up to 90° /

Grimaud, John E.
Langley Research Center.

January 1961

"March 1961."Caption title.Includes bibliographical references (p. 11).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 /

Abstract

Extracted data

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

Abstract

Extracted data

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