Laminar Boundary Layer on a Circular Cone in Supersonic Flow at a Small Angle of Attack

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1951
Accession Number
ADA380402

Entities

People

  • Franklin K. Moore

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Boundary Value Problems
  • Coefficients
  • Cross Flow
  • Differential Equations
  • Equations
  • Flow
  • Fluid Dynamics
  • Laminar Boundary Layer
  • Mach Number
  • Pressure Gradients
  • Reynolds Number
  • Secondary Flow
  • Skin Friction
  • Supersonic Flow
  • Viscous Flow

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers