Determination by the free-fall method of the longitudinal stability and control characteristics of a 1/4-scale model of the Bell XS-1 airplane at transonic speeds /

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests /

Chambers, Joseph R.
Grafton, Sue B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-15941.Includes bibliographical references (p. 19).Mode...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).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

Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 /

Fournier, Roger H.
Silvers, H. Norman.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 3, 1958."Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

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

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

Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 /

Gillis, Clarence L.
Vitale, A. James.
Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"Declassified September 4, 1956.""February 14, 1950."Includes bibliographical references (p. xx).Mod...

An investigation in the Langley 20-foot free-spinning tunnel of the spin and recovery characteristics of a 1/30-scale model of the Bell X-2 airplane /

Gale, Lawrence J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"August 12, 1949."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

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...

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

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

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests /

Chambers, Joseph R.
Grafton, Sue B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-15941.Includes bibliographical references (p. 19).Mode...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).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

Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 /

Fournier, Roger H.
Silvers, H. Norman.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 3, 1958."Includes bibliographical references (p. 9).Mode of access: Internet

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

Parks, James H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane /

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

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

Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 /

Gillis, Clarence L.
Vitale, A. James.
Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"Declassified September 4, 1956.""February 14, 1950."Includes bibliographical references (p. xx).Mod...

An investigation in the Langley 20-foot free-spinning tunnel of the spin and recovery characteristics of a 1/30-scale model of the Bell X-2 airplane /

Gale, Lawrence J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"August 12, 1949."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

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...

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

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

Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /

Penland, Jim A.
Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 18, 1955."Includes bibliographical references (p. 7).Mode of access: Internet

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests /

Chambers, Joseph R.
Grafton, Sue B.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-15941.Includes bibliographical references (p. 19).Mode...

Determination by the free-fall method of the longitudinal stability and control characteristics of a 1/4-scale model of the Bell XS-1 airplane at transonic speeds /

Abstract

Extracted data

Determination by the free-fall method of the longitudinal stability and control characteristics of a 1/4-scale model of the Bell XS-1 airplane at transonic speeds /

Abstract

Extracted data

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