By J. G. Marvin, T. J. Coakley (auth.), John J. Bertin, Jacques Periaux, Josef Ballmann (eds.)
These 3 volumes entitled Advances in Hypersonics comprise the lawsuits of the second one and 3rd Joint US/Europe brief direction in Hypersonics which came about in Colorado Springs and Aachen. the second one path used to be equipped on the US Air strength Academy, united states in January 1989 and the 3rd direction at Aachen, Germany in October 1990. the most notion of those classes was once to provide to chemists, com puter scientists, engineers, experimentalists, mathematicians, and physicists state-of-the-art lectures in clinical and technical dis ciplines together with mathematical modeling, computational tools, and experimental measurements essential to outline the aerothermo dynamic environments for area automobiles similar to the U.S. Orbiter or the eu Hermes flying at hypersonic speeds. the topics might be grouped into the next components: Phys ical environments, configuration specifications, propulsion structures (including airbreathing systems), experimental equipment for exterior and inner circulate, theoretical and numerical equipment. given that hyper sonic flight calls for hugely built-in platforms, the fast classes not just aimed to provide in-depth research of hypersonic examine and know-how but additionally attempted to increase the view of attendees to provide them the facility to appreciate the complicated challenge of hypersonic flight. many of the members within the brief classes ready a docu ment in keeping with their presentation for copy within the 3 vol umes. a few authors spent huge time and effort going well past their oral presentation to supply a top quality evaluate of the state-of-the-art of their uniqueness as of 1989 and 1991.
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Additional info for Advances in Hypersonics: Modeling Hypersonic Flows
45,34,38 47,20,20 47,20,20 40,35 40, 78 29,45 89,50 81,81 VIEGAS AND HORSTMAN (1979) MARVIN et al. (1975) COAKLEY et al. (1977) VIEGAS AND HORSTMAN (1982) COAKLEV (PVT. ) KUSSOY el al. (1980) VIEGAS AND HORSTMAN (1982) 40,32 40,32 40,32 GRID " V,
Fig. 4. Mixing length and scaled eddy viscosity from Maise and McDonald. 23 FLAT PLATE SKIN FRICTION - - VAN DRIEST COMPUTATIONS BY RUBESIN ET AL. 0 . 0 TW/TAW Fig. 5. Ability of turbulence models to predict compressibility effects: (a) adiabatic wall temperature; (b) Mach 5. and variable wall temperature. 9 IJ> I:;. 2 0 2 4 6 10 8 12 14 16 18 ReO X 10-3 Fig. 6. A comparison of experimental skin friction and heat transfer with compu· tation using a turbulence model with and without corrections for density fluctuations.
Experimental arrangements for two flows used to assess models with compressibility corrections. (b) \.. 004 u. 002 -------- ............. 001 .................. ' o 50 . _- .................. 100 x-cm 150 200 250 Fig. 13. Ogive-cylinder flow without the shock generator ring: (a) surface pressure; (b) skin friction; (c) surface heat transfer. 34 o 12 EXP -----~ C-S _ . - B-L (a} _ _ _ q-wa -~~- q-wb _ _ _ q-wc 10 88 ~ 6 4 2 0 6 (b) 5 4 \33 2 0 6 (e) 5 4 2 oL-_~~ 10 20 __ ~ ____- L____ 30 40 x-xgcm ~ 50 ____ ~ 60 __ ~ 70 Fig.
Advances in Hypersonics: Modeling Hypersonic Flows by J. G. Marvin, T. J. Coakley (auth.), John J. Bertin, Jacques Periaux, Josef Ballmann (eds.)