Investigation of Hypersonic Flow Over Blunted Plates and Cone

Rhudy, J. P.; Hiers, Robert S.; Rippey, J. O.

doi:10.21236/ad0221626

1960

DOI: 10.21236/ad0221626

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Investigation of Hypersonic Flow Over Blunted Plates and Cone

J. P. Rhudy¹,

Robert S. Hiers²,

J. O. Rippey³

Abstract: !ii i~ ~i i~ ~i ii~ ii ii~ i ii ii ii iii !! ii ii ii ii i!? ii ii ?i i~ ?! i~i i? ii ii ii i~ iii i! ii ii ii~ i ii! i~ ~i ii ii ii [!

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1965

1968

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Cited by 3 publications

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Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Blunted Cones

Wood

1968

Aeronautical Quarterly

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SummaryMeasurements have been made of laminar and transitional heat transfer rate distribution on a 15° semi-vertex angle, spherically blunted, cone at Mach numbers 8·6, 10·6 and 13·0. The laminar results are compared with theoretical predictions and good agreement is obtained with a modified form of the analysis due to Lees. Using a development of the correlation of pressure distributions previously obtained by the author, a new correlation of experimental and theoretical heat transfer results is suggested. The effect of nose bluntness on boundary layer transition has been observed both from flow visualisation and heat transfer results. It is suggested that the main factor causing nose bluntness to influence transition is the adverse pressure gradient which is induced.

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Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Blunted Cones

Wood

1968

Aeronautical Quarterly

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Comparisons of free-flight and wind-tunnel data on slender cones

Griffith¹,

Whitfield²

1965

AIAA Journal

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Reduction of stiffness and mass matrices

Guyan¹

1965

AIAA Journal

2,206

823

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Investigation of Hypersonic Flow Over Blunted Plates and Cone

Abstract: !ii i~ ~i i~ ~i ii~ ii ii~ i ii ii ii iii !! ii ii ii ii i!? ii ii ?i i~ ?! i~i i? ii ii ii i~ iii i! ii ii ii~ i ii! i~ ~i ii ii ii [!

Cited by 3 publications

References 2 publications

Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Blunted Cones

Hypersonic Laminar Heat Transfer and Boundary Layer Transition on Blunted Cones

Comparisons of free-flight and wind-tunnel data on slender cones

Reduction of stiffness and mass matrices

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