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

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 ...

Stability and control characteristics of a monoplane missile with large delta wings and various tail controls at Mach 1.90 to 2.86

Jernell, L. S.

July 1974

Wind tunnel tests were conducted to determine the stability and control characteristics of a monopla...

Experimental investigation of the transonic and supersonic flutter characteristics of the upper and lower vertical tails of an air-to-ground missile

Hanson, P. W.
Rainey, A. G.

June 1957

Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...

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

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

August 1979

The results of pressure distribution tests conducted in the Langley Unitary Plan wind tunnel are pre...

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 ...

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....

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50

Lamb, M.
Hernandez, G.
Allen, J. M.

September 1983

Tabulated body surface pressure data for two monoplane-wing missile configurations are presented and...

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...

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...

Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings

Spearman, M. L.

January 1983

The aerodynamic characteristics for a winged and wingless cruciform missile configuration were exami...

Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins

Blair, A. B., Jr.

September 1978

A wind tunnel investigation was made at free stream Mach numbers from 1.70 to 2.86 to determine the ...

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...

FREE-FLIGHT INVESTIGATION AT TRANSONIC SPEEDS OF THE STABILITY CHARACTERISTICS OF A TAILLESS MISSILE CONFIGURATION HAVING A 45 DEG SWEPTBACK WING OF ASPECT RATIO 4

Arbic, R. G.

August 1956

Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - st...

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 ...

Stability and control characteristics of a monoplane missile with large delta wings and various tail controls at Mach 1.90 to 2.86

Jernell, L. S.

July 1974

Wind tunnel tests were conducted to determine the stability and control characteristics of a monopla...

Experimental investigation of the transonic and supersonic flutter characteristics of the upper and lower vertical tails of an air-to-ground missile

Hanson, P. W.
Rainey, A. G.

June 1957

Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...

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

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

August 1979

The results of pressure distribution tests conducted in the Langley Unitary Plan wind tunnel are pre...

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 ...

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....

Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50

Lamb, M.
Hernandez, G.
Allen, J. M.

September 1983

Tabulated body surface pressure data for two monoplane-wing missile configurations are presented and...

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...

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...

Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings

Spearman, M. L.

January 1983

The aerodynamic characteristics for a winged and wingless cruciform missile configuration were exami...

Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins

Blair, A. B., Jr.

September 1978

A wind tunnel investigation was made at free stream Mach numbers from 1.70 to 2.86 to determine the ...

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...

FREE-FLIGHT INVESTIGATION AT TRANSONIC SPEEDS OF THE STABILITY CHARACTERISTICS OF A TAILLESS MISSILE CONFIGURATION HAVING A 45 DEG SWEPTBACK WING OF ASPECT RATIO 4

Arbic, R. G.

August 1956

Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - st...

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 ...

Stability and control characteristics of a monoplane missile with large delta wings and various tail controls at Mach 1.90 to 2.86

Jernell, L. S.

July 1974

Wind tunnel tests were conducted to determine the stability and control characteristics of a monopla...

Experimental investigation of the transonic and supersonic flutter characteristics of the upper and lower vertical tails of an air-to-ground missile

Hanson, P. W.
Rainey, A. G.

June 1957

Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...

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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