ESTABLISHING A CONSISTENT COMPRESSIONEXPANSION FORMULA FOR THE SUPERSONIC-HYPERSONIC REGIME,

Abstract

The paper proposes to analyze the expression for the pressure coefficient at large angles of incidence to establish a consistent formula for supersonic-hypersonic regimes, and, under certain conditions, for the impact (Newtonian) regime.

Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1964
Accession Number
AD0607543

Entities

People

  • Elie Carafoli

Organizations

  • National Air and Space Intelligence Center

Tags

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight