Static aerodynamic characteristics, pressure distributions, and RAM-air inflation of attached inflatable decelerator models at Mach 3.0 /

Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack /

Jorgensen, Leland H.
United States. National Aeronautics and Space Administration.

Issued Sept. 1977.Includes bibliographical references (p. 68-74).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

A structural merit function for aerodynamic decelerators /

Anderson, Melvin S.
Mikulas, Martin M.
Bohon, Herman L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Structural merit function for aerodynamic decelerators.Includes bibliographical references (p. 18-19...

Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 ̊to 15 /

Stallings, Robert L.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...

Aerodynamic drag and stability characteristics of towed inflatable decelerations at supersonic speeds

McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Drag and stability characteristics of a variety of reefed and unreefed parachute configurations at Mach 1.80 with an empirical correlation for supersonic Mach numbers /

Couch, Lana M.
Langley Research Center.

January 1975

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

Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators /

Bohon, Herman L.
Miserentino, Robert.
Sawyer, James Wayne, 1941-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors /

Fuller, Dennis E.
Foster, Gerald V.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical graphs."July 1963."Cover title.Includes bibl...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Measured and computed static aerodynamic characteristics of ablating conical teflon models at Mach number 14 /

Jorgensen, Leland H.
Hagen, Jack R.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 16-17).Mode of access: Internet

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

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

Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 /

Hinson, William F.
Fournier, Roger H.
Langhans, Richard A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at M...

Aerodynamic characteristics of an oblate spheroid and a sphere at Mach numbers from 1.70 to 10.49 /

Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.Includes bibliogr...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack /

Jorgensen, Leland H.
United States. National Aeronautics and Space Administration.

Issued Sept. 1977.Includes bibliographical references (p. 68-74).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

A structural merit function for aerodynamic decelerators /

Anderson, Melvin S.
Mikulas, Martin M.
Bohon, Herman L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Structural merit function for aerodynamic decelerators.Includes bibliographical references (p. 18-19...

Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 ̊to 15 /

Stallings, Robert L.
Howell, Dorothy T.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...

Aerodynamic drag and stability characteristics of towed inflatable decelerations at supersonic speeds

McShera, John T.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Drag and stability characteristics of a variety of reefed and unreefed parachute configurations at Mach 1.80 with an empirical correlation for supersonic Mach numbers /

Couch, Lana M.
Langley Research Center.

January 1975

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

Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators /

Bohon, Herman L.
Miserentino, Robert.
Sawyer, James Wayne, 1941-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors /

Fuller, Dennis E.
Foster, Gerald V.
Langley Research Center.

Prepared at Langley Research Center.Chiefly statistical graphs."July 1963."Cover title.Includes bibl...

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

Wind-tunnel investigation at Mach numbers from 0.60 to 1.20 of the static aerodynamic characteristics of a model of a possible nonlifting reentry capsule in combination with a rocket booster /

Pearson, Albin O.
Langley Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Measured and computed static aerodynamic characteristics of ablating conical teflon models at Mach number 14 /

Jorgensen, Leland H.
Hagen, Jack R.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 16-17).Mode of access: Internet

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

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

Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 /

Hinson, William F.
Fournier, Roger H.
Langhans, Richard A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at M...

Aerodynamic characteristics of an oblate spheroid and a sphere at Mach numbers from 1.70 to 10.49 /

Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.Includes bibliogr...

Static aerodynamic characteristics of a model of a typical subsonic jet-transport airplane at Mach numbers from 0.40 to 1.20 /

Brooks, Eugene N.
Blackwell, James A.
Decker, John P.
Langley Research Center.

January 1967

"NASA TM X-1345.""Langley Research Center, Langley Station, Hampton, Va.""February 1967"--Cover.Incl...

Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack /

Jorgensen, Leland H.
United States. National Aeronautics and Space Administration.

Issued Sept. 1977.Includes bibliographical references (p. 68-74).Mode of access: Internet

Wind-tunnel investigation of static aerodynamic characteristics of a 1/9-scale model of a Project Mercury capsule at mach numbers from 1.60 to 4.65 /

Shaw, David S.
Turner, Kenneth L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

A structural merit function for aerodynamic decelerators /

Anderson, Melvin S.
Mikulas, Martin M.
Bohon, Herman L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Structural merit function for aerodynamic decelerators.Includes bibliographical references (p. 18-19...

Static aerodynamic characteristics, pressure distributions, and RAM-air inflation of attached inflatable decelerator models at Mach 3.0 /

Abstract

Extracted data

Static aerodynamic characteristics, pressure distributions, and RAM-air inflation of attached inflatable decelerator models at Mach 3.0 /

Abstract

Extracted data

Related items

Related items