Hypersonic Force, Pressure, and Heat Transfer Investigations of Sharp and Blunt Slender Cones

Hypersonic Force, Pressure, and Heat Transfer Investigations of Sharp and Blunt Slender Cones PDF Author: David B. Wilkinson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 154

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Hypersonic Force, Pressure, and Heat Transfer Investigations of Sharp and Blunt Slender Cones

Hypersonic Force, Pressure, and Heat Transfer Investigations of Sharp and Blunt Slender Cones PDF Author: David B. Wilkinson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 154

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Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow

Static Pressure on Sharp and Blunt Cones in Conical and Parallel Low-density Flow PDF Author: Max Kinslow
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 78

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The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under rarefied conditions in both a uniform and a source flow field. Angle of attack of the cones was varied up to 10 deg. Pressure distributions are presented for cold-wall conditions at 18.0 = or

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 868

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A Correlation of Artifically Induced Boundary-layer Transition Data from Blunt Slender Cones at Hypersonic Speeds

A Correlation of Artifically Induced Boundary-layer Transition Data from Blunt Slender Cones at Hypersonic Speeds PDF Author: Albert H. Boudreau
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 18

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An Investigation of Laminar Heat Transfer to Slender Cones in the Hypersonic Shock Tunnel

An Investigation of Laminar Heat Transfer to Slender Cones in the Hypersonic Shock Tunnel PDF Author: Charles E. Wittliff
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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Hypersonic Rarefied Flow Over Sharp Slender Cones

Hypersonic Rarefied Flow Over Sharp Slender Cones PDF Author: Marvin I. Kussoy
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36

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Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow regime, and the results were compared with available Monte Carlo calculations. In general, the calculations predicted the magnitude of the data; however, the heat transfer and drag increased with increasing Knudsen number at a faster rate than predicted. Also the drag coefficients measured for the slender cones at high Knudsen number were higher than predicted for free molecule flow. These disagreements between theory and experiment could possibly be attributed to the simplicity of the surface interaction laws assumed in the theory. Reynolds analogy factors obtained from the experimental measurements agreed with free-molecule values and also with that obtained by the Monte Carlo technique.

Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 828

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Study of High-density Hypervelocity Flows and Similitudes

Study of High-density Hypervelocity Flows and Similitudes PDF Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 320

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Hypersonic Viscous Drag on Cones in Rarefied Flow

Hypersonic Viscous Drag on Cones in Rarefied Flow PDF Author: Marvin I. Kussoy
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20

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Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20

Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20 PDF Author: Theodore R. Creel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 42

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