Comparison of experimental and theoretical boundary-layer separation for inlets at incidence angle at low-speed conditions /

Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference /

Knechtel, Earl D. (Earl Dennis)
United States. National Aeronautics and Space Administration.

January 1959

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

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)...

Use of multiple discrete wall jets for delaying boundary layer separation /

McLean, J. D.
Herring, H. J.
Lewis Research Center.
Princeton University.

"Prepared by Princeton University ... for Lewis Research Center.""June 1974."Cover title.Includes bi...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

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

The numerical calculation of laminar boundary-layer separation /

Klineberg, John M.
Steger, Joseph L.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 31-34).Mode of ...

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of a translating-grid choked-flow inlet /

Abbott, John M.
Golladay, Richard L.
Miller, Brent A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15-16).Mode of...

Performance and boundary-layer evaluation of a sonic inlet /

Schmidt, James F.
Ruggeri, Robert S., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Theoretical surface velocity distributions on acoustic splitter geometries for an engine inlet /

Albers, James A.
Breunlin, Douglas C.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acc...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

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

Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) /

Schmidt, James F.
Todd, Carroll A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22-23).Mode of...

An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube /

Weilmuenster, K. James.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference /

Knechtel, Earl D. (Earl Dennis)
United States. National Aeronautics and Space Administration.

January 1959

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

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)...

Use of multiple discrete wall jets for delaying boundary layer separation /

McLean, J. D.
Herring, H. J.
Lewis Research Center.
Princeton University.

"Prepared by Princeton University ... for Lewis Research Center.""June 1974."Cover title.Includes bi...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets /

Hingst, Warren R.
Lewis Research Center.

January 1975

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

The numerical calculation of laminar boundary-layer separation /

Klineberg, John M.
Steger, Joseph L.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 31-34).Mode of ...

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of a translating-grid choked-flow inlet /

Abbott, John M.
Golladay, Richard L.
Miller, Brent A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15-16).Mode of...

Performance and boundary-layer evaluation of a sonic inlet /

Schmidt, James F.
Ruggeri, Robert S., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 25).Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions /

Albers, James A.
Miller, Brent A.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ac...

Theoretical surface velocity distributions on acoustic splitter geometries for an engine inlet /

Albers, James A.
Breunlin, Douglas C.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acc...

Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle /

Harvey, William D., 1934-
Harris, Julius E.
Cary, Aubrey M.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-25).Mode ...

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

Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) /

Schmidt, James F.
Todd, Carroll A.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 22-23).Mode of...

An experimental investigation of wall boundary-layer transition Reynolds numbers in an expansion tube /

Weilmuenster, K. James.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ...

Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference /

Knechtel, Earl D. (Earl Dennis)
United States. National Aeronautics and Space Administration.

January 1959

Cover title.Includes bibliographical references (p. 20-21).Mode of access: Internet

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)...

Use of multiple discrete wall jets for delaying boundary layer separation /

McLean, J. D.
Herring, H. J.
Lewis Research Center.
Princeton University.

"Prepared by Princeton University ... for Lewis Research Center.""June 1974."Cover title.Includes bi...

Comparison of experimental and theoretical boundary-layer separation for inlets at incidence angle at low-speed conditions /

Abstract

Extracted data

Comparison of experimental and theoretical boundary-layer separation for inlets at incidence angle at low-speed conditions /

Abstract

Extracted data

Related items

Related items