A THIN AIRFOIL WITH A MINIMUM AVERAGE COEFFICIENT OF HEAT TRANSFER FOR A GIVEN LIFT

Abstract

The transition to high supersonic velocities of flight leads to significant kinetic heating of the wing of an aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1962
Accession Number
AD0291718

Entities

People

  • Joy B. Gazley

Organizations

  • RAND Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Equations
  • Euler Equations
  • Government Procurement
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • Laminar Boundary Layer
  • Layers
  • Mach Number
  • Mechanics
  • Turbulent Boundary Layer
  • United States

Fields of Study

  • Physics

Technology Areas

  • Hypersonics