Accession Number:

AD0832027

Title:

AN EXPERIMENTAL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF SLENDER HYPERSONIC VEHICLES AT HIGH ANGLES OF ATTACK

Descriptive Note:

Final rept.

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

• Feldhuhn, Robert H.
• Pasiuk, Lionel

Report Date:

1968-05-01

Pagination or Media Count:

119.0

Abstract:

Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 23 power law body and two ducted-cone configurations.

Descriptors:

• *FLOW SEPARATION
• *HYPERSONIC TEST VEHICLES
• HEAT TRANSFER
• SLENDER BODIES
• DISTRIBUTION
• MOMENTS
• ANGLE OF ATTACK
• FLOW VISUALIZATION
• FLOW FIELDS
• MODEL TESTS
• PRESSURE
• HYPERSONIC CHARACTERISTICS
• CONICAL BODIES
• BLUNT BODIES
• FORCE(MECHANICS)
• WIND TUNNEL MODELS
• BODIES OF REVOLUTION

Subject Categories:

• Guided Missiles
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE