Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).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

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

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

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing /

Polhamus, Edward C.
Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

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 ...

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

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).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

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).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

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

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

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Low-subsonic-speed static stability of right-triangular-pyramid and half-cone lifting reentry configurations. /

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

Abstract:Cover title."February 1961."Aerodynamics, missiles and space vehicles; Space vehicles; Stab...

Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing /

Polhamus, Edward C.
Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Rocket-model investigation of lateral stability characteristics and power effects of a jet-engine airplane configuration with tail boom at mach numbers from 1.15 to 1.37 /

Curry, T. Bradley.
Crabill, Norman L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical re...

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 ...

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

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).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

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

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

Investigation of the low-subsonic stability and control characteristics of a 1/3-scale free-flying model of a lifting-body reentry configuration /

Hassell, James L.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 14).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

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Abstract

Extracted data

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Abstract

Extracted data

Related items

Related items