Preliminary flight evaluation of the stability and control derivatives and dynamic characteristics of the unaugmented XB-70-1 airplane including comparisons with predictions /

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Controllability of the X-15 research airplane with interim engines during high-altitude flights /

Holleman, Euclid C.
Reisert, Donald.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 10).Mode of access: Internet

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

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

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

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Summary of preliminary data derived from the XB-70 airplanes /

Andrews, William H.
Flight Research Center (U.S.)

January 1966

Work performed at Flight Research Center.Includes bibliographical references (p. 13).Mode of access:...

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...

Handling qualities of the XB-70 airplane in the landing approach.

Berry, Donald T.
Powers, Bruce G.
Flight Research Center.
United States. National Aeronautics and Space Administration.

Approach and landing performance of XB-70 aircraft.Prepared at Flight Research Center."February 1970...

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

Crane, Harold L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Simulators and computers; Stability and control.Includes bibliograp...

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 ...

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Flight investigation of a structural mode control system for the XB-70 aircraft /

Lock, Wilton P.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 22).Mode...

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Statistical analysis of landing-contact conditions for the XB-70 airplane /

Wilson, Ronald J.
Larson, Richard R.
Flight Research Center (U.S.)
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 11).Mode of access: Internet

Controllability of the X-15 research airplane with interim engines during high-altitude flights /

Holleman, Euclid C.
Reisert, Donald.
United States. National Aeronautics and Space Administration.

January 1961

"March 1961."Includes bibliographical references (p. 10).Mode of access: Internet

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

Stability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds /

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

"April 1963."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

Summary of preliminary data derived from the XB-70 airplanes /

Andrews, William H.
Flight Research Center (U.S.)

January 1966

Work performed at Flight Research Center.Includes bibliographical references (p. 13).Mode of access:...

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...

Handling qualities of the XB-70 airplane in the landing approach.

Berry, Donald T.
Powers, Bruce G.
Flight Research Center.
United States. National Aeronautics and Space Administration.

Approach and landing performance of XB-70 aircraft.Prepared at Flight Research Center."February 1970...

Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. /

Crane, Harold L.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Simulators and computers; Stability and control.Includes bibliograp...

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 ...

Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /

Yancey, Roxanah B.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircra...

Flight investigation of a structural mode control system for the XB-70 aircraft /

Lock, Wilton P.
Flight Research Center (U.S.)

January 1973

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 22).Mode...

Flight investigation to determine the effect of longitudinal characteristics on low-speed instrument operation /

DiCarlo, Daniel J.
Sommer, Robert W.
Kelly, James R.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 17).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane /

Finch, Thomas W.
Matranga, Gene J.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Preliminary flight evaluation of the stability and control derivatives and dynamic characteristics of the unaugmented XB-70-1 airplane including comparisons with predictions /

Abstract

Extracted data

Preliminary flight evaluation of the stability and control derivatives and dynamic characteristics of the unaugmented XB-70-1 airplane including comparisons with predictions /

Abstract

Extracted data

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