Attached And Separated Boundary Layers On Highly Cooled Ablating And Nonablating Models At M
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Attached And Separated Boundary Layers On Highly Cooled Ablating And Nonablating Models At M
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Author : Donald M. Kuehn
language : en
Publisher:
Release Date : 1967
Attached And Separated Boundary Layers On Highly Cooled Ablating And Nonablating Models At M written by Donald M. Kuehn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Ablation (Aerothermodynamics) categories.
Laminar Boundary Layer Separation Induced By Flares On Cylinders With Highly Cooled Boundary Layers At A Mach Number Of 15
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Author : Donald M. Kuehn
language : en
Publisher:
Release Date : 1965
Laminar Boundary Layer Separation Induced By Flares On Cylinders With Highly Cooled Boundary Layers At A Mach Number Of 15 written by Donald M. Kuehn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.
Leading Edge Bluntness And Boundary Layer Displacement Effects On Attached And Separated Laminar Boundary Layers In A Compression Corner
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Author : Michael S. Holden
language : en
Publisher:
Release Date : 1968
Leading Edge Bluntness And Boundary Layer Displacement Effects On Attached And Separated Laminar Boundary Layers In A Compression Corner written by Michael S. Holden 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.
The Effect Of Heat Transfer On Separation Of Laminar Compressible Boundary Layers
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Author : Stuart B. Savage
language : en
Publisher:
Release Date : 1962
The Effect Of Heat Transfer On Separation Of Laminar Compressible Boundary Layers written by Stuart B. Savage and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Electronic dissertations categories.
Tani's integral method (Jnl. Aero. Sci., Vol. 21, No. 7:487-504, 1954) is extended to treat laminar two-dimensional compressible boundary layers with heat transfer and arbitrary pressure gradient for both attached and separated flows. A carefully chosen one-parameter family for the velocity profiles and a universal stagnation enthalpy profile are assumed for attached flows. The accuracy of the method is examined by comparing the results with several exact numerical solutions and satisfactory agreement is obtained. For separated flows one-parameter families are assumed for both the velocity and stagnation enthalpy profiles. In this case the accuracy of the method is poor; however, suggestions are made as to how it might be improved within the present framework. (Author).
Boundary Layer Transition On Blunt Bodies With Highly Cooled Boundary Layers
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Author : Kenneth F. Stetson
language : en
Publisher:
Release Date : 1959
Boundary Layer Transition On Blunt Bodies With Highly Cooled Boundary Layers written by Kenneth F. Stetson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.