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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
Product Details :
Genre |
: Boundary layer |
Author |
: J. Leith Potter |
Publisher |
: |
Release |
: 1975 |
File |
: 36 Pages |
ISBN-13 |
: UOM:39015104951945 |
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Product Details :
Genre |
: Astronautics |
Author |
: |
Publisher |
: |
Release |
: 1966 |
File |
: 670 Pages |
ISBN-13 |
: MINN:319510005865064 |
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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
Product Details :
Genre |
: Science |
Author |
: John J. Bertin |
Publisher |
: AIAA |
Release |
: 1994 |
File |
: 644 Pages |
ISBN-13 |
: 1563470365 |
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BOOK EXCERPT:
Product Details :
Genre |
: Mechanics, Applied |
Author |
: |
Publisher |
: |
Release |
: 1974 |
File |
: 620 Pages |
ISBN-13 |
: UCAL:C2682447 |
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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.
Product Details :
Genre |
: Aeronautics |
Author |
: |
Publisher |
: |
Release |
: 1978 |
File |
: 1008 Pages |
ISBN-13 |
: UIUC:30112075601028 |
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BOOK EXCERPT:
Product Details :
Genre |
: Boundary layer |
Author |
: David F. Fisher |
Publisher |
: |
Release |
: 1982 |
File |
: 148 Pages |
ISBN-13 |
: UIUC:30112106570432 |
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BOOK EXCERPT:
Product Details :
Genre |
: Aeronautics |
Author |
: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development |
Publisher |
: |
Release |
: 1977 |
File |
: 414 Pages |
ISBN-13 |
: OSU:32435019236546 |
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BOOK EXCERPT:
Boundary-layer transition location measurements were made on a 10-deg sharp cone in 23 wind tunnels in the United States and Europe and in flight. The data were acquired at subsonic, transonic, and supersonic Mach numbers over a range of unit Reynolds numbers in an effort to obtain an improved understanding of the effect of wind tunnel flow quality on transition location. The data indicate that the transition mechanism in both wind tunnels and flight is associated with the formation of Tollmien-Schlichting waves in the laminar boundary layer. However, the location of the end of transition was found to be primarily a function of the noise under the laminar boundary of the cone surface and, within + or - 20 percent, independent of Mach number and unit Reynolds number. (Author).
Product Details :
Genre |
: Boundary layer |
Author |
: N. Sam Dougherty |
Publisher |
: |
Release |
: 1982 |
File |
: 52 Pages |
ISBN-13 |
: UOM:39015104952109 |
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BOOK EXCERPT:
Product Details :
Genre |
: |
Author |
: |
Publisher |
: |
Release |
: 199? |
File |
: 880 Pages |
ISBN-13 |
: MSU:31293017237466 |
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BOOK EXCERPT:
Product Details :
Genre |
: Boundary layer |
Author |
: Bill Harvey |
Publisher |
: |
Release |
: 1978 |
File |
: 40 Pages |
ISBN-13 |
: UIUC:30112106660258 |