A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Subsonic longitudinal and lateral-directional static aerodynamic characteristics of a general research fighter model employing a strake-wing concept

Fox, C. H., Jr.

January 1978

A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...

Stability and Control Characteristics at Subsonic Speeds of a Flat-Top Arrowhead Wing-Body Combination

Johnson, Norman S.
Buell, Donald A.

March 1959

A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...

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, J. A.
Fetterman, D. E., Jr.

April 1960

X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic spee...

Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane

Pierpont, P. K.

March 1959

Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...

Flight Test of the Lateral Stability of a 0.133-Scale Model of the Convair XFY-1 Airplane with Windmilling Propellers at Mach Numbers from 0.70 to 1.12 (TED No. NACA DE 369)

Hollinger, James A.
Mitcham, Grady L.

October 1955

A flight test of a rocket-propelled model of the Convair XFY-1 airplane was conducted to determine t...

Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane

Freeman, D. C., Jr.
Fink, M. P.

January 1969

Full scale wind tunnel investigation of lateral and longitudinal stability and control characteristi...

Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter Airplane

White, J. A.
Kraft, C. C., Jr.
Mc Laughlin, M. D.
Champine, R. A.

December 1958

Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...

A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds

Anderson, Seth B
Bray, Richard S

January 1955

This report presents the results of flight measurements of longitudinal stability and control charac...

Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well above the Wing Plane - Lateral and Directional Stability

Wetzel, Benton E.

August 1954

The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...

Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine airplane

Fink, M. P.
Greer, H. D.
Freeman, D. C., Jr.

March 1970

Full scale wind tunnel investigation of static longitudinal and lateral stability and control charac...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

Penland, J. A.
Dillon, J. L.
Hallissy, J. B.

December 1979

The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...

Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Deg Sweepback

Childs, Joan M

February 1953

Flight measurements of the stability characteristics of the Bell X-5 research airplane at 59 deg swe...

A summary of results obtained during flight simulation of several aircraft prototypes with variable-stability airplanes

Mc Neill, W. E.
Creer, B. Y.

May 1956

Dynamic lateral stability and handling data from flight simulation with F6F-3 and F-86A VARIABLE-STA...

Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees

Draper, John W.
Kuhn, Richard E.

An investigation has been made at high subsonic speeds of the aerodynamic'characteristics in pitch a...

NACA Research Memorandums

Alexander, Sidney R.

November 1948

Two rocket-powered models representative of a fighter-type airplane were investigated in flight at M...

Subsonic longitudinal and lateral-directional static aerodynamic characteristics of a general research fighter model employing a strake-wing concept

Fox, C. H., Jr.

January 1978

A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...

Stability and Control Characteristics at Subsonic Speeds of a Flat-Top Arrowhead Wing-Body Combination

Johnson, Norman S.
Buell, Donald A.

March 1959

A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...

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, J. A.
Fetterman, D. E., Jr.

April 1960

X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic spee...

Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter Airplane

Pierpont, P. K.

March 1959

Transonic wind tunnel study of static longitudinal and lateral stability and control characteristics...

Flight Test of the Lateral Stability of a 0.133-Scale Model of the Convair XFY-1 Airplane with Windmilling Propellers at Mach Numbers from 0.70 to 1.12 (TED No. NACA DE 369)

Hollinger, James A.
Mitcham, Grady L.

October 1955

A flight test of a rocket-propelled model of the Convair XFY-1 airplane was conducted to determine t...

Full-scale wind-tunnel investigation of static longtudinal and lateral characteristics of a light twin-engine airplane

Freeman, D. C., Jr.
Fink, M. P.

January 1969

Full scale wind tunnel investigation of lateral and longitudinal stability and control characteristi...

Flight Measurements of Some of the Flying Qualities and Stability Derivatives of a Supersonic Fighter Airplane

White, J. A.
Kraft, C. C., Jr.
Mc Laughlin, M. D.
Champine, R. A.

December 1958

Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...

A Flight Evaluation of the Longitudinal Stability Characteristics Associated with the Pitch-up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds

Anderson, Seth B
Bray, Richard S

January 1955

This report presents the results of flight measurements of longitudinal stability and control charac...

Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well above the Wing Plane - Lateral and Directional Stability

Wetzel, Benton E.

August 1954

The static lateral- and directional-stability characteristics of a high-speed fighter-type airplane,...

Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine airplane

Fink, M. P.
Greer, H. D.
Freeman, D. C., Jr.

March 1970

Full scale wind tunnel investigation of static longitudinal and lateral stability and control charac...

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

Penland, J. A.
Dillon, J. L.
Hallissy, J. B.

December 1979

The static longitudinal, lateral, and directional stability characteristics of a hypersonic research...

Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Deg Sweepback

Childs, Joan M

February 1953

Flight measurements of the stability characteristics of the Bell X-5 research airplane at 59 deg swe...

A summary of results obtained during flight simulation of several aircraft prototypes with variable-stability airplanes

Mc Neill, W. E.
Creer, B. Y.

May 1956

Dynamic lateral stability and handling data from flight simulation with F6F-3 and F-86A VARIABLE-STA...

Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees

Draper, John W.
Kuhn, Richard E.

An investigation has been made at high subsonic speeds of the aerodynamic'characteristics in pitch a...

NACA Research Memorandums

Alexander, Sidney R.

November 1948

Two rocket-powered models representative of a fighter-type airplane were investigated in flight at M...

Subsonic longitudinal and lateral-directional static aerodynamic characteristics of a general research fighter model employing a strake-wing concept

Fox, C. H., Jr.

January 1978

A general research fighter model was tested in the Langley 7 by 10 foot high speed tunnel at a Mach ...

Stability and Control Characteristics at Subsonic Speeds of a Flat-Top Arrowhead Wing-Body Combination

Johnson, Norman S.
Buell, Donald A.

March 1959

A wind-tunnel investigation was made to determine the longitudinal- and lateral-stability derivative...

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, J. A.
Fetterman, D. E., Jr.

April 1960

X-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic spee...

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Abstract

Extracted data

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Abstract

Extracted data

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