Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 Volume 1: Trapezoidal tail

Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing

Graves, E. B.
Fournier, R. H.

July 1974

Investigations have been conducted in the Langley 8-foot transonic pressure tunnel and the Langley U...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet

Hayes, C.
Sawyer, W. C.

July 1976

An investigation was made to determine the aerodynamic characteristics of an airbreathing missile co...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71

Couch, L. M.
Morris, W. D.

April 1968

Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry b...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 1: Trapezoidal tail

Lamb, M.
Wassum, D. L.
Babb, C. D.
Sawyer, W. C.

August 1979

The results of pressure distribution tests conducted in a wind tunnel are presented without analysis...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 3: Cranked tail

Sawyer, W. C.
Babb, C. D.
Wassum, D. L.
Lamb, M.

August 1979

The results of pressure distribution tests are presented without analysis. The test Reynolds number ...

Pressure distributions on three different cruciform aft-control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 2: Clipped delta tail

Wassum, D. L.
Lamb, M.
Babb, C. D.
Sawyer, W. C.

August 1979

Pressure coefficients were obtained in the Langley Unitary Plan wind tunnel for a wingless missile w...

A Study of Panel Loads and Centers of Pressure of Three Different Cruciform Aft-Tail Control Surfaces of a Wingless Missile from Mach 1.60 to 3.70

Trescot, C. D., Jr.
Lamb, M.

May 1980

An investigation was made of the forces and moments on the cruciform aft-tail control surfaces of a ...

Effect of fin planform on the aerodynamic characteristics of a wingless missile with AFT cruciform controls at Mach 1.60, 2.36, and 2.86

Trescot, C. D., Jr.
Foster, G. V.
Babb, C. D.

July 1973

An investigation was made in the Langley Unitary Plan wind tunnel to determine the effects of fin pl...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

Supersonic aerodynamic characteristics of a low-aspect-ratio missile model with wing and tail controls and with tails in line and interdigitated

Graves, E. B.

April 1972

A study has been made to determine the aerodynamic characteristics of a low-aspect ratio cruciform m...

Longitudinal aerodynamic characteristics at Mach 1.50 to 4.63 of a missile model employing various canards and a trailing edge flap control

Trescot, C. D., Jr.

October 1971

Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged miss...

Stability and control characteristics of a monoplannar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86

Blair, A. B., Jr.

August 1977

An experimental wind tunnel investigation has been made to determine the longitudinal and lateral ae...

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Wind-tunnel Tests of a Model of a Wingless Fin-controlled Missile to Obtain Static Stability and Control Characteristics Through a Range of Mach Numbers from 0.5 to 0.88

Burrows, Dale L
Newman, Ernest E

April 1954

An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...

Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 deg to 60 deg

Landrum, E. J.

October 1977

The tabulated results of wind tunnel pressure tests are presented without analysis. The data were ob...

Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing

Graves, E. B.
Fournier, R. H.

July 1974

Investigations have been conducted in the Langley 8-foot transonic pressure tunnel and the Langley U...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet

Hayes, C.
Sawyer, W. C.

July 1976

An investigation was made to determine the aerodynamic characteristics of an airbreathing missile co...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71

Couch, L. M.
Morris, W. D.

April 1968

Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry b...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 1: Trapezoidal tail

Lamb, M.
Wassum, D. L.
Babb, C. D.
Sawyer, W. C.

August 1979

The results of pressure distribution tests conducted in a wind tunnel are presented without analysis...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 3: Cranked tail

Sawyer, W. C.
Babb, C. D.
Wassum, D. L.
Lamb, M.

August 1979

The results of pressure distribution tests are presented without analysis. The test Reynolds number ...

Pressure distributions on three different cruciform aft-control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 2: Clipped delta tail

Wassum, D. L.
Lamb, M.
Babb, C. D.
Sawyer, W. C.

August 1979

Pressure coefficients were obtained in the Langley Unitary Plan wind tunnel for a wingless missile w...

A Study of Panel Loads and Centers of Pressure of Three Different Cruciform Aft-Tail Control Surfaces of a Wingless Missile from Mach 1.60 to 3.70

Trescot, C. D., Jr.
Lamb, M.

May 1980

An investigation was made of the forces and moments on the cruciform aft-tail control surfaces of a ...

Effect of fin planform on the aerodynamic characteristics of a wingless missile with AFT cruciform controls at Mach 1.60, 2.36, and 2.86

Trescot, C. D., Jr.
Foster, G. V.
Babb, C. D.

July 1973

An investigation was made in the Langley Unitary Plan wind tunnel to determine the effects of fin pl...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

Lamb, Milton.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 02."August 1979"--Cover.v. 1. Trapezoidal tail -- v. 2. Clipped delta tail -- v. 3....

Supersonic aerodynamic characteristics of a low-aspect-ratio missile model with wing and tail controls and with tails in line and interdigitated

Graves, E. B.

April 1972

A study has been made to determine the aerodynamic characteristics of a low-aspect ratio cruciform m...

Longitudinal aerodynamic characteristics at Mach 1.50 to 4.63 of a missile model employing various canards and a trailing edge flap control

Trescot, C. D., Jr.

October 1971

Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged miss...

Stability and control characteristics of a monoplannar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86

Blair, A. B., Jr.

August 1977

An experimental wind tunnel investigation has been made to determine the longitudinal and lateral ae...

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations

Hayes, C.

March 1983

A series of air-breathing missile configurations was investigated to provide a data base for the des...

Wind-tunnel Tests of a Model of a Wingless Fin-controlled Missile to Obtain Static Stability and Control Characteristics Through a Range of Mach Numbers from 0.5 to 0.88

Burrows, Dale L
Newman, Ernest E

April 1954

An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...

Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 deg to 60 deg

Landrum, E. J.

October 1977

The tabulated results of wind tunnel pressure tests are presented without analysis. The data were ob...

Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing

Graves, E. B.
Fournier, R. H.

July 1974

Investigations have been conducted in the Langley 8-foot transonic pressure tunnel and the Langley U...

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet

Hayes, C.
Sawyer, W. C.

July 1976

An investigation was made to determine the aerodynamic characteristics of an airbreathing missile co...

Experimental pressure distributions on a blunt lifting-entry body at Mach 3.71

Couch, L. M.
Morris, W. D.

April 1968

Wind tunnel investigation of pressure distribution on blunted 15 deg half-cone wedge lifting-entry b...

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 Volume 1: Trapezoidal tail

Abstract

Extracted data

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 Volume 1: Trapezoidal tail

Abstract

Extracted data

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