Accession Number:

AD0752018

Title:

Environmental Temperature and Aircraft Compatibility Studies,

Descriptive Note:

Corporate Author:

NAVAL AIR ENGINEERING CENTER PHILADELPHIA PA ENGINEERING DEPT (SI)

Personal Author(s):

• Gaeman,G.
• Goon,W.

Report Date:

1972-10-01

Pagination or Media Count:

77.0

Abstract:

A study of both landbased and shipboard tests of the F14A aircraft with the MK7 Jet Blast Deflector to investigate the effect of backflow of jet exhaust on the aircraft being launched and the resulting environmental temperature aft and alongside the JBD. Configuration for shipboard installation and desired mode of operation are recommended. Areas for further effort to achieve improved compatibility are also presented. Author

Descriptors:

• (*EXHAUST FLAMES
• INGESTION(ENGINES))
• (*JET AIRCRAFT
• TAKEOFF)
• EXHAUST NOZZLES
• TEMPERATURE
• DEFLECTION
• FLOW FIELDS
• AIRCRAFT CARRIERS
• WIND
• AFTERBURNERS

Subject Categories:

• Aircraft
• Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE