The Stabiwi’y of the Laminar Boundary’ Layer ~’ a Compressible Fluid

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suMM.4RY _______________________________________________ ~N~ODrC~OX ------------------------------------------sYmoM -----------------------------------------------I. PEEU~IIXART eONsIDEE.iTIOXS-------------------------2. 13ALCULATIOXOF THE LIMITS OF STABILITY OF L.WIX.AR BOUNDARYLAYER IFi AVISCOIJSf20XDCCTIVEGas. _______ 3. DESTABILIZINGIXFLUEXCEOF VISCOSITY AT T’ERY LARGE REYNOLDS XUMBERS; EXTENSION OF HEISEXBERG’S CRITERIONTO THE COMPREssIB= FLUID_______________ 4. STABILITY OF LXJIXAR BOUXDARYLAYER A-r J.ARGER~YNoLrIs NuMB~Rs---------------------------------------A. Subsonic Free-Stream Veloeity (M,< I)____ . ..-. _. B. Supersonic Free-Stream l’elocity(.llo>l) _________ 5. CRm~RIOXFORTm311NIMU.V CRITICALREYXOLDSNTCTMBER_ & PHYSICALSIGAWICANCEOFRESCLTSOFSTABILITY.kALYSIS_ A. General--------------------------------------B. EtTeet of Free-Stream Mach Number and Thermal Conditions at Sofid Surface on Stability ofLaminar Boundary Layer -------------------------C. Results of DetaiIed Stability Calculations for lJXWIated and hioninsulated Smfaees---------------D. Instability of Laminar Boundary Layer and Tram~iticmto Turbulent Flow ________________________ 7. STABKJTY OF LAMIXAR BOEXD~RY-IiATERFLOW OF .L GAS WITH A PRESSUREGRADI~NTIN THE D~RZCTIOXOF rrm FRWZ,STRZ.M _________________ _______________________ 331 33~ 332 332

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تاریخ انتشار 1997