Accession Number:

AD0475971

Title:

NOL BALLISTICS RANGE PROGRAM ON ABRES RESEARCH

Descriptive Note:

Final technical rept. 20 Oct 1964-20 Oct 1965

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

• Lankford, John L.

Report Date:

1965-10-20

Pagination or Media Count:

100.0

Abstract:

Contents Measurement of Turbulent Skin Friction on a Slender Cone Effect of High Heat Transfer Rates on Boundary Layer Transition Body Scale Effects on the Aerodynamic Characteristics of Wakes Including Edge Roughness The Effect of Heat Transfer on the Aerodynamic Characteristics of Wakes.

Descriptors:

• *REENTRY VEHICLES
• *CONICAL BODIES
• *HYPERVELOCITY PROJECTILES
• EXPERIMENTAL DATA
• SLENDER BODIES
• PERFORMANCE(ENGINEERING)
• BOUNDARY LAYER
• TURBULENT BOUNDARY LAYER
• SCALE
• SKIN FRICTION
• FREE FLIGHT MODELS
• BASE FLOW
• SABOT PROJECTILES
• REYNOLDS NUMBER
• WAKE
• BOUNDARY LAYER TRANSITION
• HYPERSONIC CHARACTERISTICS
• DRAG
• ENTHALPY
• ROUGHNESS

Subject Categories:

• Guided Missiles
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE