BASIC CONCEPTS OF EQUATIONS FOR THE AERODYNAMICS OF BODIES OF REVOLUTION,

Abstract

Aerodynamic forces and moments; the basic features of very high velocity gas flow; the basic concepts and equations for determining the flow parameters; Basic relations for determining gas parameters behind a shock wave; Results from boundary-layer and heattransfer theory.

Document Details

• Document Type: Technical Report
• Publication Date: Aug 01, 1965
• Accession Number: AD0625836

Entities

People

• Nikolai F. Krasnov

Organizations

• RAND Corporation

Tags

DTIC Thesaurus Topics

• Aerodynamic Forces
• Aerodynamics
• Bodies
• Bodies Of Revolution
• Boundaries
• Boundary Layer
• Equations
• Flow
• Fluid Dynamics
• Gas Flow
• Layers
• Revolutions
• Shock
• Shock Waves
• Waves

Fields of Study

• Physics

Readers

• Aerodynamics/Aeronautics.
• Calculus or Mathematical Analysis
• Combustion and Flow Dynamics.