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Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers by Adams, J. C, Jr., is a nonfiction available to read on EtoBox.

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Wall temperature effects on two- and three-dimensional high Reynolds number turbulent boundary layers are examined for representative high Reynolds number tunnel (HIRT) conditions relative to flight; also considered are hot-wall conditions relative to space shuttle subsonic and transonic flight during earth entry. Results show significant influences of wall-to-stagnation temperature ratio on the location of boundary-layer separation and the friction drag coefficient. The study also indicates how rapid model wall temperature during a typical testing period of 2 to 10 sec may be undesirable for HIRT testing since unsteady aerodynamic phenomena can be influenced by rapidly changing turbulent boundary-layer wall temperature levels. (Modified author abstract)

Who reads Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers?

Author

Adams, J. C, Jr.,

Publisher

Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973.

Published

1973

Language

EN

Category

nonfiction