Investigation Of Boundary Layer Transition On Flat Faced Bodies Of Revolution At High Supersonic Speeds

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Investigation Of Boundary Layer Transition On Flat Faced Bodies Of Revolution At High Supersonic Speeds

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Author : Thomas N. Canning
language : en
Publisher:
Release Date : 1957

Investigation Of Boundary Layer Transition On Flat Faced Bodies Of Revolution At High Supersonic Speeds written by Thomas N. Canning and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with categories.

Boundary Layer Transition Study Of Several Pointed Bodies Of Revolution At Supersonic Speeds

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Author : William A. Cassels
language : en
Publisher:
Release Date : 1970

Boundary Layer Transition Study Of Several Pointed Bodies Of Revolution At Supersonic Speeds written by William A. Cassels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aerodynamics, Supersonic categories.

Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fineness ratios 7, 10, and 13 at zero angle of attack for free-stream Mach numbers of 2.00, 2.75, and 4.63 and a range of Reynolds numbers based on model length of 6 to 15 X 10(to the 6 power) with and without a roughness strip. The grit method of inducing turbulence was found to provide for a nearly complete turbulent flow over the models at the lower Mach numbers and higher Reynolds numbers considered in this study while the amount of trip drag was less than 8 percent of the model drag with transition fixed. A method of interpreting sublimation data was discussed and used and the results compared well with the impact-pressure results.

Boundary Layer Transition At Supersonic Speeds

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Author : E. R. Van Driest
language : en
Publisher:
Release Date : 1961

Boundary Layer Transition At Supersonic Speeds written by E. R. Van Driest and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics, Supersonic categories.

Experiments carried out in the 12-inch supersonic wind tunnel to investigate the effect of three dimensional roughness elements (spheres) on boundary-layer transition on a 10-degree (apex angle) cone without heat transfer are described. The local Mach number for these tests was 2.71. The data show clearly that the minimum (effective) size of trip required to bring transition to its lowest Reynolds number varies power of the distance from the apex of the cone to the trip. Use of available data at other Mach numbers indicates that the Mach number influence for effective tripping is taken into account by a simple expression. Some remarks concerning the roughness variation for transition on a blunt body are made. Finally, a general criterion is introduced which gives insight to the transition phenomenon and anticipates effects of external and internal disturbances, Mach number transfer.

Boundary Layer Transition Study Of Several Pointed Bodies Of Revolution At Supersonic Speeds

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Author : William A. Cassels
language : en
Publisher:
Release Date : 1970

Boundary Layer Transition Study Of Several Pointed Bodies Of Revolution At Supersonic Speeds written by William A. Cassels and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.

Factors Affecting Transition At Supersonic Speeds

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Author : K. R. Czarnecki
language : en
Publisher:
Release Date : 1953

Factors Affecting Transition At Supersonic Speeds written by K. R. Czarnecki and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aerodynamics, Supersonic categories.

This paper surveys the available material and summarizes what is known to date about boundary-layer transition at supersonic speeds. Variables studied include Mach number, Reynolds number, pressure gradients, heat transfer, surface roughness, and angle of attack. The discussion is limited to bodies of revolution because similar reliable data for wings is lacking.

Some Experiments At High Supersonic Speeds On The Aerodynamic And Boundary Layer Transition Characteristics Of High Drag Bodies Of Revolution

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Author : Alvin Seiff
language : en
Publisher:
Release Date : 1957

Some Experiments At High Supersonic Speeds On The Aerodynamic And Boundary Layer Transition Characteristics Of High Drag Bodies Of Revolution written by Alvin Seiff and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with categories.

Experimental Investigation Of Temperature Recovery Factors On Bodies Of Revolution At Supersonic Speeds

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Author : William R. Wimbrow
language : en
Publisher:
Release Date : 1949

Experimental Investigation Of Temperature Recovery Factors On Bodies Of Revolution At Supersonic Speeds written by William R. Wimbrow and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.

Local temperature recovery factors have been measured on two bodies of revolution at Mach numbers of 2.0 and are shown to be independent of Mach number, Reynolds number, or body shape. The measured recovery factor is well represented by the square root of Prandtl number for laminar boundary layers and by the cube root of Prandtl number for turbulent boundary layers, as predicted by theory.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1968

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.

Investigations At Supersonic Speeds Of The Base Pressure On Bodies Of Revolution With And Without Sweptback Stabilizing Fins

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Author : Eugene S. Love
language : en
Publisher:
Release Date : 1952

Investigations At Supersonic Speeds Of The Base Pressure On Bodies Of Revolution With And Without Sweptback Stabilizing Fins written by Eugene S. Love and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.

Advances In Compressible Turbulent Mixing

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Author :
language : en
Publisher:
Release Date : 1992

Advances In Compressible Turbulent Mixing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Fluid dynamics categories.