Low-speed measurements of oscillatory lateral stability derivatives of a model of 60° delta-wing bomber /

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

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model /

Fisher, Lewis R.
Langley Research Center.

January 1960

"NASA TN D-232.""Langley Research Center, Langley Field, Va.""March 1960."Cover title.Includes bibli...

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

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

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Shanks, Robert E.
Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage /

Gainer, Thomas G.
Langley Research Center.

January 1961

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

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model /

Fisher, Lewis R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 24, 1958."Includes bibliographical references (p. 16).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.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

An exploratory investigation in a ballistic range of the stability derivatives of a simple airplane configuration at low supersonic speeds /

DeRose, Charles E.
Boissevain, Alfred G.
Ames Research Center.

Prepared at Ames Research Center."December 1959."Cover title.Includes bibliographical references (p....

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

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

Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 /

Sort, Barbara J.
Sommer, Simon C.
Ames Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.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

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model /

Fisher, Lewis R.
Langley Research Center.

January 1960

"NASA TN D-232.""Langley Research Center, Langley Field, Va.""March 1960."Cover title.Includes bibli...

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

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

Low-speed measurements of static and oscillatory lateral stability derivatives of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Shanks, Robert E.
Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Low-speed investigation of effects of vertical tails on the static stability characteristics of a canard-bomber configuration having a very thin wing and a slender elliptical fuselage /

Gainer, Thomas G.
Langley Research Center.

January 1961

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

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model /

Fisher, Lewis R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 24, 1958."Includes bibliographical references (p. 16).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.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

An exploratory investigation in a ballistic range of the stability derivatives of a simple airplane configuration at low supersonic speeds /

DeRose, Charles E.
Boissevain, Alfred G.
Ames Research Center.

Prepared at Ames Research Center."December 1959."Cover title.Includes bibliographical references (p....

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops /

Applin, Zachary T.
Coe, Paul L.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 63)....

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

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

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

Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 /

Sort, Barbara J.
Sommer, Simon C.
Ames Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.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

Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model /

Fisher, Lewis R.
Langley Research Center.

January 1960

"NASA TN D-232.""Langley Research Center, Langley Field, Va.""March 1960."Cover title.Includes bibli...

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

Low-speed measurements of oscillatory lateral stability derivatives of a model of 60° delta-wing bomber /

Abstract

Extracted data

Low-speed measurements of oscillatory lateral stability derivatives of a model of 60° delta-wing bomber /

Abstract

Extracted data

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