Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 /

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

"November 1959."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 02."December 1981"--Cover."Langley Research Center."Bibliography: p. 10.Mode of acc...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63 /

Babb, C. Donald.
Fuller, Dennis E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 7).Mode of access: Internet

The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations /

Mitchell, Jesse L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"January 29, 1952; Declassified July 17, 1958."Includes bibliographical references (p. 10-12).Mode o...

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 stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 /

Johnston, Patrick J.
Snyder, Curtis D.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Satellites; Space vehicles; Sta...

Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 /

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

"November 1959."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 /

Driver, Cornelius.
Spearman, M. Leroy.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 02."December 1981"--Cover."Langley Research Center."Bibliography: p. 10.Mode of acc...

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane /

Penland, Jim A.
Fetterman, Jr., David E.
Langley Research Center.

January 1960

"April 1960"--Cover.Caption title.Includes bibliographical references (p. 10-11).Mode of access: Int...

Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63 /

Babb, C. Donald.
Fuller, Dennis E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 7).Mode of access: Internet

The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations /

Mitchell, Jesse L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"January 29, 1952; Declassified July 17, 1958."Includes bibliographical references (p. 10-12).Mode o...

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 stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20 /

Ferris, James C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).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

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Abstract

Extracted data

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Abstract

Extracted data

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