The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects /

Maddalon, Dal V.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 8).M...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

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

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

Aerodynamic characteristics of a modified cone : conical-frustum entry configuration at Mach 6.0 /

Ashby, George C.
Staylor, W. Frank.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."June 1968."Includes bibliographical references (p. 8).Mode of access: Internet

A preliminary investigation of modified blunt 13° half-cone re-entry configurations at subsonic speeds /

Kenyon, George C.
Edwards, George G.
Ames Research Center.

January 1961

"March 1961."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry /

Putnam, Lawrence E. (Lawrence Elwood)
Brooks, Cuyler W.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle /

Mugler, John P.
Olstad, Walter B.
United States. National Aeronautics and Space Administration.

"December 1960."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects /

Maddalon, Dal V.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 8).M...

Aerodynamic characteristics of towed cones used as decelerators at mach numbers rom 1.57 to 4.65 /

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

Cover title." December 1961."Aerodynamics, missiles and space vehicles;Atmospheric entry.Includes bi...

Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"December 1959."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 /

Monta, William J.
Czarnecki, K. R.
Howard, Paul W.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration /

Ware, George M.
Langley Research Center.

January 1962

"December 1962."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

January 1961

"February 1961."Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5 /

Covell, Peter F.
Howell, Dorothy T.
Walker, Ira J.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 7).Mode of access: Inter...

Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees /

Treon, Stuart L.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Space vehicles; S...

Subsonic aerodynamic characteristics of disk re-entry configurations with elliptic cross sections and thickness-diameter ratios of 0.225 and 0.325 /

Demele, Fred A.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

"May 1961."Cover title.Includes bibliographical references (p. 9-10).Mode of access: Internet

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Abstract

Extracted data

The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13° half cone at Mach numbers to 0.90 /

Abstract

Extracted data

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