The determination of the aerodynamic characteristics of an ogive-cylinder body in subsonic curved, incompressible flow and an assessment of the effect of flow curvature

The development of a drag prediction method for simple forebody shapes at supersonic speeds using a simplified flow model

El-Borai, M
Hatfield Polytechnic (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1980

SIGLEAvailable from British Library Document Supply Centre- DSC:D37692/81 / BLDSC - British Library ...

NIJMBEROF 3.85

R. Jack
John R. Jack

January 1951

An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...

NACA Technical Reports

Ferri, Antonio

January 1951

The method of characteristics has been applied for the determination of the supersonic-flow properti...

The drag of cones, plates, and hemispheres in the wake of a forebody in subsonic flow /

Heinrich, Helmut G., 1910-1979 author.
Haak, Eugene L., author.
University of Minnesota. Department of Aerospace Engineering and Mechanics, sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor.

The drag of a number of bodies having some resemblance to aerodynamic deceleration devices was measu...

Analysis of experiments to measure body vortices in curved flow

Ward, B.
Lloyd, A
Admiralty Marine Technology Establishment (AMTE), Gosport (United Kingdom)

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:0696.5605(ARE-TM(UHU)--88305) / BLDS...

Numerical techniques for predicting aerodynamic characteristics of bodies

Deo, H.S
Cranfield Inst. of Tech. (United Kingdom)

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D69320/86 / BLDSC - British Library ...

An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen.

Tinling, Bruce E.
Allen, Clyde Q.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 /

Jorgensen, Leland H. (Leland Howard)
Nelson, Edgar R.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

Experimental aerodynamic characteristics for a cylindrical body of revolution with various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 /

Jorgensen, Leland H. (Leland Howard)
Nelson, Edgar R.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

The aerodynamic force characteristics of flow past a single square cylinder at different Reynolds numbers.

Shamsul Islam (4494607)
Ghazala Nazeer (4494601)
Zhou Chao Ying (4494604)
Ziaul Islam (238906)
Raheela Manzoor (4494610)

October 2017

<p>The aerodynamic force characteristics of flow past a single square cylinder at different Reynolds...

Some data on the effect of thrust on drag at subsonic speeds

Rylands, H.D.
Aeroplane and Armament Experimental Establishment, Boscombe Down (UK)

January 1962

SIGLELD:7369.27(AAEE-Res--309) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Surface flow angles on an ogive cylinder at angle of attack in supersonic flow /

Vaughn, Harold R. author.
George, Oscar L., Jr., author.
Sandia Corporation.
U.S. Atomic Energy Commission.

The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach ...

The aerodynamic chararcteristics of power-law bodies in continuum and transitional hypersonic flow

Regan, J.D
Westby, M.F.
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1989

Report also known as BR--111667Available from British Library Document Supply Centre- DSC:8670.19(RA...

Aerodynamic characteristics of 2-, 3-, and 4-, caliber tangent-ogive cylinders with nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 at Mach numbers from 0.6 to 4.0 /

Butler, Carroll B., author.
Pallas, Spiros Georgios, 1942-. author.
Sears, Edward S. (Edward Seldon), 1943-. author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element: 62601F, JON: 670E-02-01.""Final Report for the period March 1971 to February 1976....

The Subsonic Aerodynamic Characteristics of a Body of Revolution — A Revised Experiment.

P. A. T. Christopher
Z. Hussain^^^^^ *̂
P. A. T. Christopher
Z. Hussain
C. T. Shavk̂

January 1984

'The riews expressed herein are those of the authors alone and do not necessarily represent tho...

The development of a drag prediction method for simple forebody shapes at supersonic speeds using a simplified flow model

El-Borai, M
Hatfield Polytechnic (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1980

SIGLEAvailable from British Library Document Supply Centre- DSC:D37692/81 / BLDSC - British Library ...

NIJMBEROF 3.85

R. Jack
John R. Jack

January 1951

An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...

NACA Technical Reports

Ferri, Antonio

January 1951

The method of characteristics has been applied for the determination of the supersonic-flow properti...

The drag of cones, plates, and hemispheres in the wake of a forebody in subsonic flow /

Heinrich, Helmut G., 1910-1979 author.
Haak, Eugene L., author.
University of Minnesota. Department of Aerospace Engineering and Mechanics, sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor.

The drag of a number of bodies having some resemblance to aerodynamic deceleration devices was measu...

Analysis of experiments to measure body vortices in curved flow

Ward, B.
Lloyd, A
Admiralty Marine Technology Establishment (AMTE), Gosport (United Kingdom)

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:0696.5605(ARE-TM(UHU)--88305) / BLDS...

Numerical techniques for predicting aerodynamic characteristics of bodies

Deo, H.S
Cranfield Inst. of Tech. (United Kingdom)

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D69320/86 / BLDSC - British Library ...

An Investigation of the normal-force and vortex-wake characteristics of an Ogive-cylinder body at subsonic speeds Bruce E. Tinling and Clyde Q. Allen.

Tinling, Bruce E.
Allen, Clyde Q.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 /

Jorgensen, Leland H. (Leland Howard)
Nelson, Edgar R.
Ames Research Center.

January 1975

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

Experimental aerodynamic characteristics for a cylindrical body of revolution with various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 /

Jorgensen, Leland H. (Leland Howard)
Nelson, Edgar R.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 7).Mode of acce...

The aerodynamic force characteristics of flow past a single square cylinder at different Reynolds numbers.

Shamsul Islam (4494607)
Ghazala Nazeer (4494601)
Zhou Chao Ying (4494604)
Ziaul Islam (238906)
Raheela Manzoor (4494610)

October 2017

<p>The aerodynamic force characteristics of flow past a single square cylinder at different Reynolds...

Some data on the effect of thrust on drag at subsonic speeds

Rylands, H.D.
Aeroplane and Armament Experimental Establishment, Boscombe Down (UK)

January 1962

SIGLELD:7369.27(AAEE-Res--309) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Surface flow angles on an ogive cylinder at angle of attack in supersonic flow /

Vaughn, Harold R. author.
George, Oscar L., Jr., author.
Sandia Corporation.
U.S. Atomic Energy Commission.

The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach ...

The aerodynamic chararcteristics of power-law bodies in continuum and transitional hypersonic flow

Regan, J.D
Westby, M.F.
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1989

Report also known as BR--111667Available from British Library Document Supply Centre- DSC:8670.19(RA...

Aerodynamic characteristics of 2-, 3-, and 4-, caliber tangent-ogive cylinders with nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 at Mach numbers from 0.6 to 4.0 /

Butler, Carroll B., author.
Pallas, Spiros Georgios, 1942-. author.
Sears, Edward S. (Edward Seldon), 1943-. author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element: 62601F, JON: 670E-02-01.""Final Report for the period March 1971 to February 1976....

The Subsonic Aerodynamic Characteristics of a Body of Revolution — A Revised Experiment.

P. A. T. Christopher
Z. Hussain^^^^^ *̂
P. A. T. Christopher
Z. Hussain
C. T. Shavk̂

January 1984

'The riews expressed herein are those of the authors alone and do not necessarily represent tho...

The development of a drag prediction method for simple forebody shapes at supersonic speeds using a simplified flow model

El-Borai, M
Hatfield Polytechnic (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1980

SIGLEAvailable from British Library Document Supply Centre- DSC:D37692/81 / BLDSC - British Library ...

NIJMBEROF 3.85

R. Jack
John R. Jack

January 1951

An experimental investigation to determine the aerodynamic characteristics of a slender body of revo...

NACA Technical Reports

Ferri, Antonio

January 1951

The method of characteristics has been applied for the determination of the supersonic-flow properti...

The determination of the aerodynamic characteristics of an ogive-cylinder body in subsonic curved, incompressible flow and an assessment of the effect of flow curvature

Abstract

Extracted data

The determination of the aerodynamic characteristics of an ogive-cylinder body in subsonic curved, incompressible flow and an assessment of the effect of flow curvature

Abstract

Extracted data

Related items

Related items