Accession Number:

AD0857474

Title:

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

Descriptive Note:

Technical Report

Corporate Author:

NAVAL WEAPONS CENTER CHINA LAKE CA CHINA LAKE United States

Personal Author(s):

Report Date:

1969-06-01

Pagination or Media Count:

318.0

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.

Descriptors:

• SYMPOSIA
• AERODYNAMICS
• BALLISTICS
• AERODYNAMICS
• NUMERICAL ANALYSIS
• COMPRESSIBLE FLOW
• NONEQUILIBRIUM FLOW
• BLUNT BODIES
• SUPERSONIC CHARACTERISTICS
• ABLATION
• TURBULENCE
• TURBULENT BOUNDARY LAYER
• BLUNT BODIES
• LEADING EDGES
• HALOCARBON PLASTICS
• HEAT TRANSFER
• MASS TRANSFER
• DRAG
• SPIKES
• EROSION

Subject Categories:

• Ammunition and Explosives
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE