Proceedings of the Navy Symposium on Aeroballistics (8th) 6, 7, 8 May 1969 Naval Weapons Center, Corona Laboratories, Corona, California. Volume 2

Abstract

Contents: Applications of the time-dependent technique for the computation of compressible flows; Nonequilibrium flow over blunt bodies using method of integral relations; Supersonic laminar and turbulent ablation studies with teflon; Recent progress in the calculation of turbulent boundary layers; An experimental investigation of the compressible turbulent boundary layer with a favorable pressure gradient; An experimental Reynolds analogy for the highly cooled turbulent boundary layer; The effect of flow field irregularities on swept leading edge heat transfer; An experimental study of mass addition effects in the near wake; Isothermal leading edges; and Spikes as a means of reducing drag and rain erosion of blunt bodies at supersonic speeds.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0857474

Entities

Organizations

  • Naval Air Weapons Station China Lake

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundary Layer
  • Chemical Reactions
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Geometry
  • Heat Transfer
  • Hydrodynamics
  • Mechanics
  • Physics Laboratories
  • Pressure Distribution
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion science or combustion engineering.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers