Accession Number:

AD0836259

Title:

WIND TUNNEL TESTING TECHNIQUES FOR INTEGRATED AIRFRAME-EXHAUST NOZZLE SYSTEMS.

Descriptive Note:

Final rept. 1 May 67-2 May 68,

Corporate Author:

NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV

Personal Author(s):

• Bonner, E.
• Nixon, J. A.

Report Date:

1968-07-01

Pagination or Media Count:

272.0

Abstract:

Descriptors:

• *NOZZLE GAS FLOW
• *EXHAUST NOZZLES
• WIND TUNNEL MODELS
• JET MIXING FLOW
• FLOW FIELDS
• INTERACTIONS
• SUPERSONIC CHARACTERISTICS
• THRUST
• DRAG
• EXHAUST GASES
• MODEL TESTS
• MATHEMATICAL MODELS
• CONVERGENT DIVERGENT NOZZLES
• PLUG NOZZLES
• INSTRUMENTATION
• DOORS

Subject Categories:

• Test Facilities, Equipment and Methods
• Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE