USE OF THE SMALL PERTURBATIONS METHOD TO CALCU- LATE NONADIABATIC FLOW AROUND A FLAT PLATE USING A SUPERSONIC FLOW OF IDEAL GAS,

Document Details

Document Type
Technical Report
Publication Date
Apr 24, 1963
Accession Number
AD0415664

Entities

People

  • I.f. Shakhnov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Gas Flow
  • Mathematical Analysis
  • Mathematics
  • Perturbations
  • Supersonic Flow

Technology Areas

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