Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Water landing characteristics of a model of a winged reentry vehicle /

Stubbs, Sandy M.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 10.Mode of access: Internet

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Calculation of the longitudinal aerodynamic characteristics of STOL aircraft with externally-blown jet-augmented flaps /

Dillenius, Marnix F. E., 1938-
Spangler, Selden B.
Mendenhall, M. R.
Ames Research Center.
Nielsen Engineering & Research.

January 1974

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions /

Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-14).Mode of...

Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap /

Parlett, Lysle P.
Shivers, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept /

Andrews, Earl H.
Pinckney, S. Z. (Shimer Zane), 1934-
Agnone, Anthony M.
Langley Research Center.

January 1975

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

Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock /

Cole, Gary L.
Willoh, Ross G.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 26-27).Mode of...

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...

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 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...

Analytical study of takeoff and landing performance for a jet STOL transport configuration with full-span, externally blown, triple-slotted flaps /

Washington, Harold P.
Gibbons, John T.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 18-19).M...

Water landing characteristics of a model of a winged reentry vehicle /

Stubbs, Sandy M.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 10.Mode of access: Internet

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Calculation of the longitudinal aerodynamic characteristics of STOL aircraft with externally-blown jet-augmented flaps /

Dillenius, Marnix F. E., 1938-
Spangler, Selden B.
Mendenhall, M. R.
Ames Research Center.
Nielsen Engineering & Research.

January 1974

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Bibliogr...

Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions /

Bober, Lawrence J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-14).Mode of...

Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap /

Parlett, Lysle P.
Shivers, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept /

Andrews, Earl H.
Pinckney, S. Z. (Shimer Zane), 1934-
Agnone, Anthony M.
Langley Research Center.

January 1975

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

Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock /

Cole, Gary L.
Willoh, Ross G.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 26-27).Mode of...

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...

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 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...

Analytical study of takeoff and landing performance for a jet STOL transport configuration with full-span, externally blown, triple-slotted flaps /

Washington, Harold P.
Gibbons, John T.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 18-19).M...

Water landing characteristics of a model of a winged reentry vehicle /

Stubbs, Sandy M.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 10.Mode of access: Internet

Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane /

Grantham, William D.
Deal, Perry L.
Nguyen, Luat T.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Abstract

Extracted data

Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions /

Abstract

Extracted data

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