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Author :
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
Download or read book Transition Fixing for Hypersonic Flow written by and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James R. Sterrett
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (25 download)
Download or read book Transition Fixing for Hypersonic Flow written by James R. Sterrett and published by . This book was released on 1967 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael Hodge McCloskey
Publisher :
ISBN 13 :
Total Pages : 662 pages
Book Rating : 4.:/5 (346 download)
Download or read book A study of boundary layer transition on outgassing cones in hypersonic flow written by Michael Hodge McCloskey and published by . This book was released on 1971 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. L. Boerrigter
Publisher :
ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (11 download)
Download or read book On the Effect of Flowfield Non-uniformities on Boundary Layer Transition in Hypersonic Flow written by H. L. Boerrigter and published by . This book was released on 1995 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : M. R. Malik
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Boundary Layer Transition in Hypersonic Flows written by M. R. Malik and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. M. Charbonnier
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Contribution to the Study of Gap Induced Boundary Layer Transition in Hypersonic Flow written by J. M. Charbonnier and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Oliver Taylor
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (111 download)
Download or read book Effects of Surface Roughness on Boundary Layer Transition in a Hypersonic Flow written by Oliver Taylor and published by . This book was released on 2018 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 738 pages
Book Rating : 4.3/5 (91 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Kenneth F. Stetson
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.3/5 (91 download)
Download or read book Comments on Hypersonic Boundary-layer Transition written by Kenneth F. Stetson and published by . This book was released on 1990 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is a survey paper on the subject of hypersonic boundary-layer transition. Part 1 discusses boundary-layer stability theory, hypersonic boundary-layer stability experiments, and a comparison between theory and experiment. Part 2 contains comments on how many configuration and flow parameters influence transition. Part 3 discusses some additional general aspects of transition. Part 4 discusses problems of predicting transition and comments on three prediction methods. Part 5 contains some general guidelines for prediction methodology. Keywords: Boundary layer transition, Boundary layer stability, Hypersonic boundary layers.
Author : D. I. A. Poll
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book The Effect of Wing Sweep Back Upon Transition in Hypersonic Flow written by D. I. A. Poll and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Francesco Avallone
Publisher : Youcanprint
ISBN 13 : 8891187836
Total Pages : 189 pages
Book Rating : 4.8/5 (911 download)
Download or read book Application of non-intrusive experimental techniques to roughness-induced transition in hypersonic flows written by Francesco Avallone and published by Youcanprint. This book was released on 2015-04-30 with total page 189 pages. Available in PDF, EPUB and Kindle. Book excerpt: The application of non-intrusive experimental techniques is a break-through in the comprehension of the physical mechanisms governing roughness-induced transition in hypersonic flows. In this thesis, IR Thermography, Planar and Tomographic Particle Image Velocimetry are applied. They show a great potentiality in quantifying the most relevant flow features upstream and downstream of three-dimensional roughness elements. Particularly, non-intrusive measurements of the two-dimensional and three-dimensional velocity flow fields are reported and discussed.
Author : John J. Bertin
Publisher : AIAA
ISBN 13 : 9781563470363
Total Pages : 644 pages
Book Rating : 4.4/5 (73 download)
Download or read book Hypersonic Aerothermodynamics written by John J. Bertin and published by AIAA. This book was released on 1994 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer. Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design considerations. Includes sample exercises and homework problems. Annotation copyright by Book News, Inc., Portland, OR
Author : Mark Vladimir Morkovin (|d)
Publisher :
ISBN 13 :
Total Pages : 152 pages
Book Rating : 4.3/5 (91 download)
Download or read book Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Traveling Bodies written by Mark Vladimir Morkovin (|d) and published by . This book was released on 1969 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. L. Nagel
Publisher :
ISBN 13 :
Total Pages : 190 pages
Book Rating : 4.:/5 (227 download)
Download or read book Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack written by A. L. Nagel and published by . This book was released on 1966 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical and experimental investigation has been made of boundary layer transition at angle of attack in hypersonic flow. A new method of calculating laminar flow stability has been developed that is more general than previous methods. The method employs the timewise integration of perturbation equations derived from the complete Navier-Stokes equations for two-dimensional flow of a compressible fluid with variable transport properties. The present calculations are for perturbations about a known steady flow. The perturbations are assumed to be sinusoidal in the streamwise direction, but no restriction is known that would prevent the streamwise wave form from being arbitrary, as are the vertical distributions and the time variations. The sinusoidal wave assumption greatly reduces the amount of computer time required and simplifies the interpretation of the results. Nonlinear terms are easily retained with the present method, but nonlinear calculations are not physically correct when perturbations are required to be sinusoidal. For this reason, nonlinear terms were deleted for all calculations presented. The experimental program was conducted at Mach numbers of 6, 8, and 10. The models included blunt and sharp flat plates and a 75-degree swept delta wing with sharp leading edges.
Author : Richard K. Matthews
Publisher :
ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.3/5 (91 download)
Download or read book Heat-transfer and Flow-field Tests of the McDonnell Douglas-Martin Marietta Space Shuttle Configurations written by Richard K. Matthews and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Martin Marietta were conducted at Mach numbers 8 and 10.5. Test conditions provided both Mach number and Reynolds number simulation for typical ascent and reentry trajectories. This report provides a comprehensive analysis of the major test results and also presents data comparisons with theoretical calculations. Specific areas covered are ascent heating and shock interference, booster reentry heating and flow fields, and orbiter reentry analysis which includes leeside heating, windward shock angles and flow fields, windward surface heating, and boundary-layer transition.
Author : William A. Cassels
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)
Download or read book Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds written by William A. Cassels and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Author :
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (227 download)
Download or read book Hypersonic Boundary Layer Transition Experiments written by and published by . This book was released on 1980 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: New hypersonic wind tunnel data have been obtained to investigate boundary layer transition, with primary emphasis given to tip bluntness and angle of attack effects. The rearward displacement of transition on the cone frustum due to tip bluntness was found to be quite sensitive to free stream Mach number as well as the entropy layer swallowing by the boundary layer. At the highest Mach number obtained in these experiments (M = 9.3), the length of laminar flow could be extended to about nine times the length of laminar flow of a sharp cone at identical conditions. The sensitivity of the maximum rearward displacement of transition with free stream Mach number appeared to be primarily related to local Reynolds number reduction because of pressure losses across the bow shock. Low transition Reynolds numbers typically found on nosetips, extended onto the front portion of the cone frustum. It appears that the still unexplained low transition Reynolds numbers associated with blunt bodies in hypersonic flow includes not only the nosetip region, but the forward portion of the cone frustum. Transition location was found to be sensitive to small changes in angle of attack, and both the sharp and blunt tips produced a rearward movement of transition on the windward ray at small angles of attack. A low supersonic flared nozzle closely duplicated the hypersonic pressure and heat transfer distributions over the nose region of a blunt body.
