Fluid Dynamics, Volume 9Plenum., 1976 - American periodicals |
Contents
Influence of the Unit Reynolds Number on Transition in a Supersonic Boundary Layer | 625 |
Laminar Boundary Layer and Its Stability in Weak Polymer Solutions | 632 |
Effect of Heaving on Filtration Beneath Hydrotechnical Structures I R Basovich | 641 |
Copyright | |
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1976 Plenum Publishing adiabatic index Akad Akademii Nauk SSSR angle approximation article is available axis axisymmetric body boundary conditions boundary layer bubble calculated characteristic coefficient component computations constant coordinate corresponding cross section curves cylinder density dependence determined dimensionless distribution electronic energy equilibrium experimental fluid function gasdynamic hypersonic inertial waves injection integral curves interaction investigation ionization Izvestiya Akademii Nauk liquid LITERATURE CITED Mach number Mach wave magnetic field mechanical medium Mekhanika Zhidkosti method microfilming Moscow motion nozzle obtained Original article submitted P₁ parameters particles perturbations photocopying plane Plenum Publishing Corporation pressure problem profiles R₁ recording or otherwise region retrieval system Reynolds number Russian self-similar shock wave solution stagnation point stream function supersonic surface temperature thermal tion Translated from Izvestiya transmitted transonic turbulent values velocity viscous wall West 17th Street written permission Zhidk Zhidkosti i Gaza zone