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Author : Seymour M. Bogdonoff
Release : 1955
Genre : Boundary layer
Kind : eBook
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Book Synopsis Some Experimental Studies of the Separation of Supersonic Turbulent Boundary Layers ... by : Seymour M. Bogdonoff
Download or read book Some Experimental Studies of the Separation of Supersonic Turbulent Boundary Layers ... written by Seymour M. Bogdonoff. This book was released on 1955. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Seymour M. Bogdonoff
Release : 1975
Genre : Aerodynamics, Supersonic
Kind : eBook
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Book Synopsis Research on Supersonic Turbulent Separated and Reattached Flows by : Seymour M. Bogdonoff
Download or read book Research on Supersonic Turbulent Separated and Reattached Flows written by Seymour M. Bogdonoff. This book was released on 1975. Available in PDF, EPUB and Kindle. Book excerpt: Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.
Author : Jain-Ming Wu
Release : 1976
Genre : Aerodynamics
Kind : eBook
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Book Synopsis Experimental Study on High Subsonic Turbulent Flow Incipient Separation by : Jain-Ming Wu
Download or read book Experimental Study on High Subsonic Turbulent Flow Incipient Separation written by Jain-Ming Wu. This book was released on 1976. Available in PDF, EPUB and Kindle. Book excerpt: For flow over a two-dimensional ramp compression corner case, an experimental investigation to determine the incipient separation was carried out at Mach numbers between 0.55 and 0.9 and Reynolds numbers (based on undisturbed boundary layer thickness) between 350,000 and 690,000. Detailed surface pressure, pitot traversing and oil flow data were obtained for each ramp angle case. Two-dimensionality of the ramp compression corners was verified by the surface oil flow. A major finding of this study is that the incipient separation ramp angle is relatively independent of Mach number and Reynolds number within the range studied. The incipient separation ramp angle was found to be about 22.5 degrees.
Author : William D. Bachalo
Release : 1977
Genre :
Kind : eBook
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Book Synopsis Experiments on Transonic and Supersonic Turbulent Boundary Layer Separation by : William D. Bachalo
Download or read book Experiments on Transonic and Supersonic Turbulent Boundary Layer Separation written by William D. Bachalo. This book was released on 1977. Available in PDF, EPUB and Kindle. Book excerpt:
Author : S. M. Bogdonoff
Release : 1975
Genre :
Kind : eBook
Book Rating : /5 ( reviews)
Book Synopsis Research on Supersonic Turbulent Separated and Reattached Flows by : S. M. Bogdonoff
Download or read book Research on Supersonic Turbulent Separated and Reattached Flows written by S. M. Bogdonoff. This book was released on 1975. Available in PDF, EPUB and Kindle. Book excerpt: Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the high Reynolds number Mach 3 facility. The experimental programs concentrated on phenomena associated with incipient separation and separation of turbulent boundary layers over a large Reynolds number range. The reattachment phenomena of a shear layer was also studied in great depth.
