STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack up to 90 Degrees

Grimaud, J. E.

March 1961

Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...

STATIC STABILITY AND CONTROL CHARACTERISTICS AT LOW-SUBSONIC SPEEDS OF A LENTICULAR REENTRY CONFIGURATION

Ware, G. M.

December 1960

Static stability and control characteristics of manned lenticular reentry configuration at low subso...

Aerodynamic characteristics of some lifting reentry concepts applicable to transatmospheric vehicle design studies

Spearman, M. L.

December 1984

The aerodynamic characteristics of some lifting reentry concepts are examined with a view to the app...

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

Kenyon, G. C.
Sutton, F. B.

July 1961

Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.9

TRANSONIC INVESTIGATION OF THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIONWING-BODY CONFIGURATIONS AT ANGLES OF ATTACK AROM 0 DEG TO 90 DEG

Brooks, C. W., Jr.
Putnam, L. E.
Trescot, C. D., Jr.

June 1963

Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration

STATIC LONGTIDUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5 DEG SWEEPBACK AND 45 DEG DIHEDRAL AT A MACH NUMBER OF 6.2 AND ANGLES OF ATTACK UP TO 20 DEG

Mayo, E. E.

October 1959

Static longitudinal stability characteristics of blunted glider reentry configuratio

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.

February 1960

An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...

Research on blunt-faced entry configurations at angles of attack between 60 deg and 90 deg

Phillips, W. H.

September 1960

Stability and control of blunt reentry configurations at angles of attack between 60 and 90 degree

Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration

Foster, Gerald V.

December 1959

An investigation has been conducted to determine the longitudinal stability and control characterist...

Investigation of Several Blunt Bodies to Determine Transonic Aerodynamic Characteristics Including Effects of Spinning and of Extendible Afterbody Flaps and Some Measurements of Unsteady Base Pressures

Fisher, L. R.
Di Camillo, J. R.

January 1959

Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...

Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects

Maddalon, D. V.

March 1966

Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach...

EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG

Foster, G. V.

February 1961

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles ...

Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane

Pittman, J. L.
Dillon, J. L.

August 1978

The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...

Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6

Nelms, W. P., Jr.
Thomas, C. L.

November 1971

Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft...

Low-Subsonic Measurements of the Static Stability and Control and Oscillatory Stability Derivatives of a Proposed Reentry Vehicle Having an Extensible Heat Shield for High-Drag Reentry

Boisseau, Peter C.
Johnson, Joseph L., Jr.

August 1961

A low-speed investigation has been made to determine the static and oscillatory longitudinal and lat...

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack up to 90 Degrees

Grimaud, J. E.

March 1961

Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...

STATIC STABILITY AND CONTROL CHARACTERISTICS AT LOW-SUBSONIC SPEEDS OF A LENTICULAR REENTRY CONFIGURATION

Ware, G. M.

December 1960

Static stability and control characteristics of manned lenticular reentry configuration at low subso...

Aerodynamic characteristics of some lifting reentry concepts applicable to transatmospheric vehicle design studies

Spearman, M. L.

December 1984

The aerodynamic characteristics of some lifting reentry concepts are examined with a view to the app...

THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92

Kenyon, G. C.
Sutton, F. B.

July 1961

Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.9

TRANSONIC INVESTIGATION OF THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF LOW-ASPECT-RATIONWING-BODY CONFIGURATIONS AT ANGLES OF ATTACK AROM 0 DEG TO 90 DEG

Brooks, C. W., Jr.
Putnam, L. E.
Trescot, C. D., Jr.

June 1963

Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration

STATIC LONGTIDUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5 DEG SWEEPBACK AND 45 DEG DIHEDRAL AT A MACH NUMBER OF 6.2 AND ANGLES OF ATTACK UP TO 20 DEG

Mayo, E. E.

October 1959

Static longitudinal stability characteristics of blunted glider reentry configuratio

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.

February 1960

An investigation of the low-subsonic-speed static longitudinal stability and control characteristics...

Research on blunt-faced entry configurations at angles of attack between 60 deg and 90 deg

Phillips, W. H.

September 1960

Stability and control of blunt reentry configurations at angles of attack between 60 and 90 degree

Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration

Foster, Gerald V.

December 1959

An investigation has been conducted to determine the longitudinal stability and control characterist...

Investigation of Several Blunt Bodies to Determine Transonic Aerodynamic Characteristics Including Effects of Spinning and of Extendible Afterbody Flaps and Some Measurements of Unsteady Base Pressures

Fisher, L. R.
Di Camillo, J. R.

January 1959

Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angl...

Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects

Maddalon, D. V.

March 1966

Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach...

EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG

Foster, G. V.

February 1961

Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles ...

Aerodynamic characteristics at Mach 6 of a wing-body concept for a hypersonic research airplane

Pittman, J. L.
Dillon, J. L.

August 1978

The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed...

Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6

Nelms, W. P., Jr.
Thomas, C. L.

November 1971

Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft...

Low-Subsonic Measurements of the Static Stability and Control and Oscillatory Stability Derivatives of a Proposed Reentry Vehicle Having an Extensible Heat Shield for High-Drag Reentry

Boisseau, Peter C.
Johnson, Joseph L., Jr.

August 1961

A low-speed investigation has been made to determine the static and oscillatory longitudinal and lat...

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack up to 90 Degrees

Grimaud, J. E.

March 1961

Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90...

STATIC STABILITY AND CONTROL CHARACTERISTICS AT LOW-SUBSONIC SPEEDS OF A LENTICULAR REENTRY CONFIGURATION

Ware, G. M.

December 1960

Static stability and control characteristics of manned lenticular reentry configuration at low subso...

Aerodynamic characteristics of some lifting reentry concepts applicable to transatmospheric vehicle design studies

Spearman, M. L.

December 1984

The aerodynamic characteristics of some lifting reentry concepts are examined with a view to the app...

STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

Abstract

Extracted data

STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

Abstract

Extracted data

Related items

Related items