Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Boundary Layer Stability Analysis For Sharp Cones At Zero Angle Of Attack
Download Boundary Layer Stability Analysis For Sharp Cones At Zero Angle Of Attack full books in PDF, epub, and Kindle. Read online Boundary Layer Stability Analysis For Sharp Cones At Zero Angle Of Attack ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Boundary-Layer Stability Analysis for Sharp Cones at Zero Angle-of-Attack by :
Download or read book Boundary-Layer Stability Analysis for Sharp Cones at Zero Angle-of-Attack written by and published by . This book was released on 1986 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The stability characteristics of an uncooled sharp cone at zero angle of attack have been calculated at an edge Mach number of 6.8 and a stagnation temperature of 728 K (1310 R) using spatial normal modes. Transformed flat-plate boundary-layer profiles were used for the mean flow. By a consideration of both two-dimensional and oblique waves, it has been determined that instability at this Mach number is primarily a two-dimensional second-mode instability. Comparisons with available stability experiments show that the calculated unstable frequencies were present in the experiments, but the measured amplification rates differ from the calculated. A band of unstable high frequencies above the second-mode region that starts at about R=1400 is not accounted for by the theory. Comparisons of amplitude-growth curves for both cones and flat plates at March numbers 4.5, 5.8 and 6.8 show that the most unstable normal modes on a cone have at least as much total growth as on a flat plate at Mach 4.5 and more total growth at the other two Mach numbers. Keywords: Boundary layer stability; Hypersonic linear stability theory; Hypersonic cone stability.
Book Synopsis Boundary-layer Stability Analysis for Sharp Cones at Zero Angle-of-attack by : Mack Leslie M.
Download or read book Boundary-layer Stability Analysis for Sharp Cones at Zero Angle-of-attack written by Mack Leslie M. and published by . This book was released on 1986 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Stability of the Compressible Boundary Layer on a Sharp Cone at Zero Angle of Attack by : G. Gasperas
Download or read book The Stability of the Compressible Boundary Layer on a Sharp Cone at Zero Angle of Attack written by G. Gasperas and published by . This book was released on 1987 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Three-dimensional Laminar Boundary-layer Analysis of Upwash Patterns and Entrained Vortex Formation on Sharp Cones at Angle of Attack by : John C. Adams (Jr.)
Download or read book Three-dimensional Laminar Boundary-layer Analysis of Upwash Patterns and Entrained Vortex Formation on Sharp Cones at Angle of Attack written by John C. Adams (Jr.) and published by . This book was released on 1971 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: Application of three-dimensional inviscid and viscous (laminar boundary layer) analyses for cold wall hypersonic flows over sharp cones at incidence is presented relative to experimental data, showing surface upwash angles and entrained vortex formation leading to crossflow-induced boundary-layer transition. Three-dimensional neutral inviscid stability theory for stationary disturbances is used to calculate the angular orientation of the entrained vortices in the boundary layer while a maximum crossflow Reynolds number concept is applied for correlation of the onset to vortex formation due to crossflow instability.
Book Synopsis Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range by : J. Leith Potter
Download or read book Boundary-layer Transition on Cones Near Mach One in an Aeroballistic Range written by J. Leith Potter and published by . This book was released on 1975 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The feasibility of determining Reynolds numbers of boundary layer transition on sharp, 10-deg, semiangle cones at slightly supersonic free-stream Mach numbers, 1.04 = or
Book Synopsis Stability of a Supersonic Boundary Layer on a Sharp Cone at a Small Angle of Attack by : Deifallah A. Dajeh
Download or read book Stability of a Supersonic Boundary Layer on a Sharp Cone at a Small Angle of Attack written by Deifallah A. Dajeh and published by . This book was released on 1988 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M[mathematical Symbol for Infinity] by : George G. Mateer
Download or read book Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M[mathematical Symbol for Infinity] written by George G. Mateer and published by . This book was released on 1972 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted on 5 deg and 15 deg half-angle sharp cones at wall-to-total-temperature ratios of 0.08 to 0.4, and angles of attack from 0 deg to 20 deg. The results indicate that (1) transition Reynolds numbers decrease with decreasing temperature ratio, (2) local transition Reynolds numbers decrease from the windward to the leeward side of the model, and (3) transition data on the windward ray of cones can be correlated in terms of the crossflow velocity gradient, momentum thickness Reynolds number, local Mach number, and cone half-angle.
Book Synopsis Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects by : Arloe Wesley Mayne (Jr.)
Download or read book Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects written by Arloe Wesley Mayne (Jr.) and published by . This book was released on 1972 with total page 114 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 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 by : Michael C. Fischer
Download or read book An Experimental Investigation of Boundary-layer Transition on a 10 ̊half-angle Cone at Mach 6.9 written by Michael C. Fischer 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 on nose cones at hypersonic speeds.
Book Synopsis The Analysis and Calculation of the Three-Dimensional Boundary Layer Over a Sharp Cone at Angle of Attack by :
Download or read book The Analysis and Calculation of the Three-Dimensional Boundary Layer Over a Sharp Cone at Angle of Attack written by and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comments on Hypersonic Boundary-layer Transition by : Kenneth F. Stetson
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.
Book Synopsis Boundary Layer Flows Over Sharp and Spherically Blunted Cones at Angle of Attack to Supersonic Nonuniform Free Streams. Volume I. Analysis and Results by : Michael C. Frieders
Download or read book Boundary Layer Flows Over Sharp and Spherically Blunted Cones at Angle of Attack to Supersonic Nonuniform Free Streams. Volume I. Analysis and Results written by Michael C. Frieders and published by . This book was released on 1973 with total page 131 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods have been developed to solve the problem of laminar boundary layers on sharp and spherically blunt cones at angle of attack to nonuniform supersonic free streams. A three-dimensional boundary-layer solution is used to solve sharp cone problems and the afterbody of blunt cone problems. An axisymmetric boundary-layer solution is used to solve the axisymmetric region of blunt cones. An existing implicit finite-difference numerical scheme was used to solve both the axisymmetric and three-dimensional boundary-layer equations. A modified inverse method for solving the inviscid flow field is used to provide edge properties for the axisymmetric region of blunt cones. Normalized skin friction and heat transfer coefficients for a sharp cone in two-dimensional shear flow increase downstream relative to conical flow values. (Modified author abstract).
Book Synopsis Effects of Mass Transfer Into Laminar and Turbulent Boundary Layers Over Cones at Angle of Attack by : Michael C. Frieders
Download or read book Effects of Mass Transfer Into Laminar and Turbulent Boundary Layers Over Cones at Angle of Attack written by Michael C. Frieders and published by . This book was released on 1975 with total page 260 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M Infinite by : George G. Mateer
Download or read book Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M Infinite written by George G. Mateer and published by . This book was released on 1972 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Aerothermodynamics by : John J. Bertin
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
Book Synopsis Boundary Layer Flows Over Sharp and Spherically Blunted Cones at Angle of Attack to Supersonic Nonuniform Free Streams by : Michael C. Frieders
Download or read book Boundary Layer Flows Over Sharp and Spherically Blunted Cones at Angle of Attack to Supersonic Nonuniform Free Streams written by Michael C. Frieders and published by . This book was released on 1973 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download Effects of Wall Cooling and Angle of Attack on Boundary-layer Transition on Sharp Cones at M[mathematical Symbol for Infinity] PDF Online Free](https://books.google.com/books/content/images/frontcover/cSw9OUS9IiQC?fife=w200-h370)
