Accession Number:

AD0436796

Title:

ENGINEERING JOURNAL (SELECTED ARTICLES).

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-03-23

Pagination or Media Count:

61.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE