1973-02-01

External Blowing Flap Technology on the USAF McDonnell Douglas YC-15 730915

The YC-15 will be the first aircraft to employ the externally blown flap (EBF)-powered lift system. Since the success of the aircraft to a large extent is dependent on the proper functioning of this system, considerable effort is going into its design. The present paper discusses some of the fundamental aerodynamic considerations which led to the selection of the specific flap configuration and presents resulting aerodynamic characteristics. Structural design criteria for the system and methods of analysis are covered, as are details of the flap-actuating system and structure.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Technical Basis For The STOL Characteristics Of The McDonnell Douglas/USAF YC-15 Prototype Airplane

730366

View Details

TECHNICAL PAPER

Status Review - YC-15 Advanced Medium STOL Prototype

760540

View Details

TECHNICAL PAPER

STABILITY AND CONTROL OF PILOTED AIRCRAFT AT HIGH ALTITUDES

550189

View Details

X