Accession Number : AD0436796


Title :   ENGINEERING JOURNAL (SELECTED ARTICLES).


Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO


Report Date : 23 Mar 1964


Pagination or Media Count : 61


Abstract : Contents: Hypersonich Flow Past Slender Blunt Elliptic Cones; Laminar Boundary Layer with Reaction Front; Development of Plane-Parallel Boundary Layer in the Neighborhood of the Critical Point of a Blunt Body, set in Motion Impulsively; On the Nature of Flow in the Stagnation region; On Plasma Acceleration by a Megnetic Field; On the Behavior of Heated Plates and Sloping Shells in a Gas Flow; The Equation of Three Velocities for a Shock Tube. (Author)


Descriptors :   *FLUID FLOW , USSR , HYPERSONIC FLOW , SLENDER BODIES , BLUNT BODIES , CONICAL BODIES , DELTA WINGS , SHOCK WAVES , SEPARATION , LAMINAR BOUNDARY LAYER , FLAT PLATE MODELS , AERODYNAMIC HEATING , HEAT TRANSFER , GAS FLOW , INJECTION , COOLING , BOUNDARY LAYER TRANSITION , MOMENTUM , TURBULENT BOUNDARY LAYER , STAGNATION POINT , SUPERSONIC FLOW , PLASMAS(PHYSICS) , MAGNETOHYDRODYNAMICS , MAGNETIC FIELDS , ACCELERATION , CYLINDRICAL BODIES , SHELLS(STRUCTURAL FORMS) , AEROELASTICITY , MATHEMATICAL ANALYSIS


Distribution Statement : APPROVED FOR PUBLIC RELEASE