The effects of nose bluntness on the pressure fluctuations measured on 15 deg and 20 deg cone-cylinders at transonic speeds

Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypersonic flows

Sehgal, A. K.
Singh, D. J.
Tiwari, S. N.

May 1991

Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of f...

An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic mach numbers

Cleary, J. W.

August 1965

Pressure distribution and flow fields of blunted cones at hypersonic Mach number

Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air

Intrieri, P. F.

January 1966

Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...

The effects of some variations in launch- vehicle nose shape on steady and fluctuating pressures at transonic speeds

Coe, C. F.

March 1962

Effects of variations in launch vehicle nose configuration on steady and fluctuating pressures at tr...

Analytic Study of Induced Pressure on Long Bodies of Revolution with Varying Nose Bluntness at Hypersonic Speeds

VanHise, Vernon

January 1961

Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...

Pressure distributions and aerodynamic characteristics of 90 deg and 15 deg blunted cones in nitrogen and helium at Mach 20

Watson, R. D.
Miller, C. G., III
Creel, T. R., Jr.
Maddalon, D. V.

March 1968

Wind tunnel tests on pressure distribution, and shock shapes of conical blunted bodies moving at sup...

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4

Sommer, Simon C
Perkins, Edward W
Jorgensen, Leland H

January 1958

Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...

An Experimental Investigation of the Flow over Blunt-Nosed Cones at a Mach Number of 5.8

Machell, Reginald M.
O'Bryant, William T.

June 1956

Shock shapes were observed and static pressures were measured on spherically-blunted cones at a nomi...

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg

Shaw, D. S.
Fuller, D. E.
Babb, C. D.

May 1963

Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...

Pressure distributions on 140 deg, 160 deg, and 180 deg cones at Mach numbers from 2.30 to 4.63 and angles of attack from 0 deg to 20 deg

Tudor, D. H.
Campbell, J. F.

May 1969

Surface pressure distribution on spherical blunted cones, and correlation of Mach numbers, cone angl...

Experimental base pressures on 9 deg spherically blunted cones at Mach numbers from 10.5 to 20

Miller, C. G., III

October 1968

Base pressure measurements at angle of attack for spherically blunted cones at hypersonic spee

Effects of angle of attack and bluntness on the shock-layer properties of a 15 deg cone at a Mach number of 10.6

Cleary, J. W.

November 1968

Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speed

Aerodynamic characteristics of a spherically blunted 25 deg cone at a Mach number of 20

Harris, J. E.

August 1967

Aerodynamic characteristics and pressure distributions of spherically blunted 25 degree cone investi...

Effect of nose bluntness and controlled roughness on the flow on two hypersonic inlet center bodies without cowling at mach 5.98

Cubbage, J. M.

July 1965

Nose bluntness and roughness effect of flow on all-external-compression hypersonic inlet bodie

Stagnation and static pressures on a nose-mounted 15 deg conical probe with various forebody configurations

Coates, E. M., Jr.

August 1966

Pressure distribution data at subsonic and transonic speeds for calibrating hypersonic conical press...

Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypersonic flows

Sehgal, A. K.
Singh, D. J.
Tiwari, S. N.

May 1991

Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of f...

An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic mach numbers

Cleary, J. W.

August 1965

Pressure distribution and flow fields of blunted cones at hypersonic Mach number

Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air

Intrieri, P. F.

January 1966

Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...

The effects of some variations in launch- vehicle nose shape on steady and fluctuating pressures at transonic speeds

Coe, C. F.

March 1962

Effects of variations in launch vehicle nose configuration on steady and fluctuating pressures at tr...

Analytic Study of Induced Pressure on Long Bodies of Revolution with Varying Nose Bluntness at Hypersonic Speeds

VanHise, Vernon

January 1961

Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...

Pressure distributions and aerodynamic characteristics of 90 deg and 15 deg blunted cones in nitrogen and helium at Mach 20

Watson, R. D.
Miller, C. G., III
Creel, T. R., Jr.
Maddalon, D. V.

March 1968

Wind tunnel tests on pressure distribution, and shock shapes of conical blunted bodies moving at sup...

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4

Sommer, Simon C
Perkins, Edward W
Jorgensen, Leland H

January 1958

Experimental drag measurements at zero angle of attack for various theoretical minimum drag nose sha...

An Experimental Investigation of the Flow over Blunt-Nosed Cones at a Mach Number of 5.8

Machell, Reginald M.
O'Bryant, William T.

June 1956

Shock shapes were observed and static pressures were measured on spherically-blunted cones at a nomi...

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg

Shaw, D. S.
Fuller, D. E.
Babb, C. D.

May 1963

Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics ...

Pressure distributions on 140 deg, 160 deg, and 180 deg cones at Mach numbers from 2.30 to 4.63 and angles of attack from 0 deg to 20 deg

Tudor, D. H.
Campbell, J. F.

May 1969

Surface pressure distribution on spherical blunted cones, and correlation of Mach numbers, cone angl...

Experimental base pressures on 9 deg spherically blunted cones at Mach numbers from 10.5 to 20

Miller, C. G., III

October 1968

Base pressure measurements at angle of attack for spherically blunted cones at hypersonic spee

Effects of angle of attack and bluntness on the shock-layer properties of a 15 deg cone at a Mach number of 10.6

Cleary, J. W.

November 1968

Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speed

Aerodynamic characteristics of a spherically blunted 25 deg cone at a Mach number of 20

Harris, J. E.

August 1967

Aerodynamic characteristics and pressure distributions of spherically blunted 25 degree cone investi...

Effect of nose bluntness and controlled roughness on the flow on two hypersonic inlet center bodies without cowling at mach 5.98

Cubbage, J. M.

July 1965

Nose bluntness and roughness effect of flow on all-external-compression hypersonic inlet bodie

Stagnation and static pressures on a nose-mounted 15 deg conical probe with various forebody configurations

Coates, E. M., Jr.

August 1966

Pressure distribution data at subsonic and transonic speeds for calibrating hypersonic conical press...

Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypersonic flows

Sehgal, A. K.
Singh, D. J.
Tiwari, S. N.

May 1991

Hypersonic flows over cones and straight biconic configurations are calculated for a wide range of f...

An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic mach numbers

Cleary, J. W.

August 1965

Pressure distribution and flow fields of blunted cones at hypersonic Mach number

Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in air

Intrieri, P. F.

January 1966

Static and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reyno...

The effects of nose bluntness on the pressure fluctuations measured on 15 deg and 20 deg cone-cylinders at transonic speeds

Abstract

Extracted data

The effects of nose bluntness on the pressure fluctuations measured on 15 deg and 20 deg cone-cylinders at transonic speeds

Abstract

Extracted data

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