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 /

Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).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, L. M.

February 1975

An investigation was conducted at Mach 1.80 in the Langley 4-foot supersonic pressure tunnel to dete...

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 of cross type parachutes /

Niccum, R. J., author.
Gutenkauf, Robert. author.
Haak, E. L., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
United States. Air Force. Systems Command. issuing body.
University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor.

"February 1965."Includes bibliograpical references (page 30).Air Force Contract No.Mode of access: I...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range /

Foughner, James T.
Alexander, William C. (William Campbell)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 /

Morris, Odell A.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68-37854.Cover title.Includes bibliographical references (p. 7)...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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 ...

Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

Drag characteristics and dynamic stability in descent of a rotary parachute tested in a vertical tunnel /

Burk, Sanger M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Aerodynamic characteristics of parachutes at mach numbers from 1.6 to 3 /

Maynard, Julian D.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft safety and noise.Includes bibliographical references.Mode of access:...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).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, L. M.

February 1975

An investigation was conducted at Mach 1.80 in the Langley 4-foot supersonic pressure tunnel to dete...

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 of cross type parachutes /

Niccum, R. J., author.
Gutenkauf, Robert. author.
Haak, E. L., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
United States. Air Force. Systems Command. issuing body.
University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor.

"February 1965."Includes bibliograpical references (page 30).Air Force Contract No.Mode of access: I...

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range /

Foughner, James T.
Alexander, William C. (William Campbell)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 /

Morris, Odell A.
Mack, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68-37854.Cover title.Includes bibliographical references (p. 7)...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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 ...

Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds /

Stallings, Robert L.
Watson, Carolyn B.
Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Langley Research Center.""July 1980"--Cover.Includes bibliographical references.Mode of access: Int...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Exploratory investigation of the aerodynamic characteristics of a biwing vehicle at Mach 20.3 /

Bernot, Peter T.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 4...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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