FURTHER INVESTIGATION OF HEATING RATES TO SPHERICAL AND CYLINDRICAL BODIES IN A 1/10 SCALE ATLAS VERNIER ROCKET ENGINE EXHAUST,

Abstract

Object: To determine the stagnation point heating rate to spherical and cylindrical bodies of the same diameter at various locations in the highly expanded exhaust jet of a scale vernier rocket.

Document Details

Document Type
Technical Report
Publication Date
Mar 11, 1959
Accession Number
AD0831414

Entities

People

  • R. J. Sergeant

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Bodies
  • Cylindrical Bodies
  • Diameters
  • Engines
  • Geometric Forms
  • Geometry
  • Rocket Engines
  • Rockets
  • Stagnation Point
  • Vernier Rocket Engines

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Rocket Propulsion.