ENGINEERING PHYSICS (SELECTED ARTICLES)

Abstract

Experiments on Heat Transfer of a Supersonic Gas Flow in a Circular Tube at High Temperature Gradients; Solution of an Equation of Gas Motion in a Rectangular Channel with Friction and Heat Transfer; Heat and Mass Transfer in Evaporation Processes.

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Document Details

Document Type
Technical Report
Publication Date
Mar 21, 1963
Accession Number
AD0402472

Entities

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Air Temperature
  • Boundary Layer
  • Differential Equations
  • Equations
  • Experimental Data
  • Gas Flow
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • High Temperature
  • Laminar Flow
  • Mach Number
  • Mass Transfer
  • Phase Transformations
  • Pressure Distribution
  • Stagnation Temperature
  • Temperature Gradients

Fields of Study

  • Chemistry
  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight