Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

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

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

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

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).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

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° /

Robinson, Ross B.
Howard, Paul W.
Langley Research Center.

January 1960

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

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

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

January 1960

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

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

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

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).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...

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

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

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Shaw, David S.
Henderson, William P.
Langley Research Center.

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

Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails /

Lockwood, Vernard E.
Thompson, Wilson E.
Langley Research Center.

January 1964

"November 1964."Includes bibliographical references (p. 10).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

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° /

Robinson, Ross B.
Howard, Paul W.
Langley Research Center.

January 1960

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

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /

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

January 1960

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

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

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

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).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...

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

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

Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location /

Bielat, Ralph P.
Pierpont, P. Kenneth.
Langley Research Center.

January 1960

"December 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Abstract

Extracted data

Low-speed longitudinal stability characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /

Abstract

Extracted data

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