AERODYNAMIC FORCE ANALYSIS. VOLUME I

Abstract

Aerodynamic Force Analysis methods and technology from an extensive bibliography, originally prepared as an internal reference for the U. S. Army Missile Command, is presented in conjunction with definitive guidance for use and applicability. An altitude range from 0 to 400,000 feet and a Mach number range from low subsonic through oribital-re-entry level hypersonic is encompassed, with appropriate continuum, slip and free molecule flow treatments.

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1966
Accession Number
AD0802293

Entities

People

  • Branimir D. Djordjevic

Organizations

  • Auburn University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Energy Transfer
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Froude Number
  • Geometry
  • Hydrodynamics
  • Mechanical Properties
  • Physics Laboratories
  • Stratified Fluids
  • Thermal Conductivity
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Library and Information Science
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight