THE RESISTANCE OF A FLAT PLATE LOCATED NORMAL TO THE FLOW OF GREATLY RAREFIED GAS (O SOPROTIVLENII PLOSKOI PLASTNYI, RASPOLOZHENNOI NORMALNO K POTOKU SILNO RAZREZHENNOGO GAZA)

Abstract

A method is presented for calculating the aerodynamic properties of a flat plate of any given shape at arbitrary values of the accommodation coefficient in a rarefied gas flow. First-time collisions of free-stream and reflected molecules are considered, with the effect of attenuation of the reflected flow on free-stream flow taken into account. The presence of the arbitrary accommodation coefficient means that the velocity of a reflected molecule cannot be neglected at the time of collision with a free-stream molecule, and this leads to a complex collision integral. The method is based on calculating the function of the effect of molecules reflected from an elementary surface upon the aerodynamic characteristics of the other elementary surface. A detailed scheme for computer calculation by means of the Monte Carlo method was developed. The results of numerical calculations of the aerodynamic characteristics of a square plate for various values of the accommodation coefficient are presented as an illustrative example.

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Document Details

Document Type
Technical Report
Publication Date
Sep 15, 1967
Accession Number
AD0673760

Entities

People

  • V. A. Perepukhov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Drag
  • Air Force
  • Coefficients
  • Collisions
  • Flow
  • Foreign Technology
  • Free Stream
  • Gas Flow
  • Gases
  • Hypersonic Flow
  • Integrals
  • Molecules
  • Monte Carlo Method
  • Rarefied Gases
  • Resistance
  • Translations

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Information Retrieval
  • Plasma Physics / Magnetohydrodynamics