Near-Free Molecule Drag of Slender Cones,

Abstract

A systematic theoretical and empirical framework is for the study and correlation of aerodynamic drag information is an important application of the methodology of rarefied gas dynamics. In this paper a flight regime is considered for a slender pointed cone where the first effects on drag of intermolecular collisions between gas molecules which have already struck a body surface, and freestream molecules, appear. The phenomena discussed here correspond to hypersonic reentry into the upper atmosphere, where the first corrections to the traditional free-molecule drag coefficient are likely to be significant. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1970
Accession Number
AD0731251

Entities

People

  • D. R. Willis

Organizations

  • RAND Corporation

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Drag
  • Atmospheres
  • Coefficients
  • Collisions
  • Drag
  • Dynamics
  • Fluid Dynamics
  • Gas Dynamics
  • Gases
  • Molecules
  • Physics
  • Rarefied Gas Dynamics
  • Rarefied Gases

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Fluid Mechanics and Fluid Dynamics.
  • Quantum Chemistry

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight