Accession Number:

AD0701728

Title:

THRUST AUGMENTATION CONSIDERATIONS FOR STOL AND EXTENDED CRUISE PROPULSION.

Descriptive Note:

Final rept.,

Corporate Author:

AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Campbell,William S.

Report Date:

1969-11-01

Pagination or Media Count:

25.0

Abstract:

The application of thrust augmentation concepts to short take-off and landing STOL aircraft propulsion is described for some typical installations. Aerodynamic and ejector thrust effects are treated separately so that the performance of the ejector-powered wing can be calculated as that of a jet-flapped airfoil and the ejector thrust components then added. Some considerations on the performance of the ejector-powered wing in cruise are included. A program for ejector calculations is given. Author

Descriptors:

• (*SHORT TAKEOFF AIRCRAFT
• *THRUST AUGMENTATION)
• AERODYNAMIC CHARACTERISTICS
• PERFORMANCE(ENGINEERING)
• LEVEL FLIGHT
• INJECTION

Subject Categories:

• VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE