Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
An Experimental And Analytical Investigation Of Hypersonic Inlet Boundary Layers
Download An Experimental And Analytical Investigation Of Hypersonic Inlet Boundary Layers full books in PDF, epub, and Kindle. Read online An Experimental And Analytical Investigation Of Hypersonic Inlet Boundary Layers ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers: Data reduction program and tabulated experimental data by : J. F. Stroud
Download or read book An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers: Data reduction program and tabulated experimental data written by J. F. Stroud and published by . This book was released on 1965 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed boundary layer surveys were made on four axisymmetric compression surface models simulating typical hypersonic inlet compression surfaces at free stream Mach numbers ranging from 4 to 8. The four models were designed to provide isentropic compression at design Mach numbers of 5, 6, 8 and 10. The Mach 8 design model had provisions for wall cooling. Quantitative heat transfer measurements were made on the Mach 8 model at free stream Mach numbers of 5, 6, and 8. Two existing turbulent boundary layer theories were modified to account for the various phenomena found to be of importance in hypersonic boundary layers. Theoretical results from these methods were correlated with the experimental data. A significant observation of the present program is the powerful favorable effect of centrifugal force phenomena on boundary layer development in continuous adverse pressure gradients. It was found that these effects become more pronounced with increasing Mach number and reductions in free stream Reynolds number.
Book Synopsis An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers. Volume Ii. Data Reduction Program and Tabulated Experimental Data by : John F. Stroud
Download or read book An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers. Volume Ii. Data Reduction Program and Tabulated Experimental Data written by John F. Stroud and published by . This book was released on 1965 with total page 409 pages. Available in PDF, EPUB and Kindle. Book excerpt: For abstract see AD-621 343.
Book Synopsis An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers by : J. F. Stroud
Download or read book An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers written by J. F. Stroud and published by . This book was released on 1965 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed boundary layer surveys were made on four axisymmetric compression surface models simulating typical hypersonic inlet compression surfaces at free stream Mach numbers ranging from 4 to 8. The four models were designed to provide isentropic compression at design Mach numbers of 5, 6, 8 and 10. The Mach 8 design model had provisions for wall cooling. Quantitative heat transfer measurements were made on the Mach 8 model at free stream Mach numbers of 5, 6, and 8. Two existing turbulent boundary layer theories were modified to account for the various phenomena found to be of importance in hypersonic boundary layers. Theoretical results from these methods were correlated with the experimental data. A significant observation of the present program is the powerful favorable effect of centrifugal force phenomena on boundary layer development in continuous adverse pressure gradients. It was found that these effects become more pronounced with increasing Mach number and reductions in free stream Reynolds number.
Book Synopsis An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers by : John F. Stroud
Download or read book An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers written by John F. Stroud and published by . This book was released on 1965 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed boundary layer surveys were made on four axisymmetric compression surface models simulating typical hypersonic inlet compression surfaces at free stream Mach numbers ranging from 4 to 8. The four models were designed to provide isentropic compression at design Mach numbers of 5, 6, 8 and 10. The Mach 8 design model had provisions for wall cooling. Quantitative heat transfer measurements were made on the Mach 8 model at free stream Mach numbers of 5, 6, and 8. Two existing turbulent boundary layer theories were modified to account for the various phenomena found to be of importance in hypersonic boundary layers. Theoretical results from these methods were correlated with the experimental data. A significant observation of the present program is the powerful favorable effect of centrifugal force phenomena on boundary layer development in continuous adverse pressure gradients. It was found that these effects become more pronounced with increasing Mach number and reductions in free stream Reynolds number.
Book Synopsis Investigation of Flow Fields Within Large-scale Hypersonic Inlet Models by : A. Vernon Gnos
Download or read book Investigation of Flow Fields Within Large-scale Hypersonic Inlet Models written by A. Vernon Gnos and published by . This book was released on 1973 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt: Analytical and experimental investigations were conducted to determine the internal flow characteristics in model passages representative of hypersonic inlets for use at Mach numbers to about 12. The passages were large enough to permit measurements to be made in both the core flow and boundary layers. The analytical techniques for designing the internal contours and predicting the internal flow-field development accounted for coupling between the boundary layers and inviscid flow fields by means of a displacement-thickness correction. Three large-scale inlet models, each having a different internal compression ratio, were designed to provide high internal performance with an approximately uniform static-pressure distribution at the throat station. The models were tested in the Ames 3.5-Foot Hypersonic Wind Tunnel at a nominal free-stream Mach number of 7.4 and a unit free-stream Reynolds number of 8.86 X one million per meter.
Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 732 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research and Technology Program Digest by : United States. National Aeronautics and Space Administration
Download or read book Research and Technology Program Digest written by United States. National Aeronautics and Space Administration and published by . This book was released on with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government-wide Index to Federal Research & Development Reports by :
Download or read book Government-wide Index to Federal Research & Development Reports written by and published by . This book was released on 1965 with total page 954 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research and Technology Program Digest Flash Index by :
Download or read book Research and Technology Program Digest Flash Index written by and published by . This book was released on 1967 with total page 794 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow by : JEROME. PERSH
Download or read book An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow written by JEROME. PERSH and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow by : Jerome Persh
Download or read book An Analytical Investigation of Turbulent Boundary Layer Heat Transfer Coefficients for Supersonic and Hypersonic Flow written by Jerome Persh and published by . This book was released on 1955 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Analytical Studies in Continuum Hypersonic Flow by : Ting Yi Li
Download or read book Experimental and Analytical Studies in Continuum Hypersonic Flow written by Ting Yi Li and published by . This book was released on 1965 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analytical studies in continuum hypersonic flow carried out are reviewed and summarized in the present report. Also summarized is the progress made in the originally envisaged investigation of torsion-rod flexures for dynamic stability tests in hypersonic wind tunnels. The theoretical studies include investigations into inviscid hypersonic flow, hypersonic viscous-inviscid interaction, and binary boundary layer flows. (Author).
Book Synopsis Starting Phenomena for Hypersonic Inlets with Thick Turbulent Boundary Layers at Mach 6 by : Theodore J. Goldberg
Download or read book Starting Phenomena for Hypersonic Inlets with Thick Turbulent Boundary Layers at Mach 6 written by Theodore J. Goldberg and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory by : Michael C. Fischer
Download or read book Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory written by Michael C. Fischer and published by . This book was released on 1971 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel investigation of laminar, transitional, and turbulent boundary layer profiles on wedge at hypersonic speed to confirm theoretical analysis.
Book Synopsis Investigation of Hypersonic Inlet Shock-wave Boundary Layer Interaction. Part Ii. Continuous Flow Test and Analyses by : Paul H Kutschenreuter (Jr)
Download or read book Investigation of Hypersonic Inlet Shock-wave Boundary Layer Interaction. Part Ii. Continuous Flow Test and Analyses written by Paul H Kutschenreuter (Jr) and published by . This book was released on 1966 with total page 263 pages. Available in PDF, EPUB and Kindle. Book excerpt: The computational procedure developed in Phase I for estimating laminar boundary layer properties through impinging shock induced laminar boundary layer interactions was modified to account for entropy change of the inviscid streamlines in that isentropic assumptions were used in the initial formulation. Perturbation studies on the effects of wall shear on interaction length have identified the importance of the profile shape factor in such calculations. A Users' Manual for the laminar computational program is contained. Three incident shock models were designed for use in the experimental program conducted in the Ames 3.5 Foot Hypersonic Tunnel. Aided by analysis of the experimental data, a simplified flow model was formulated for the case of a two-dimensional turbulent boundary layer incident shock interaction. (Author).
