Browse Publications Technical Papers 660733
1966-02-01

Aerodynamic Considerations for Engine Inlet Design for Subsonic High Bypass Fan Engines 660733

Consideration is given the manner in which inlet throat Mach number. cowl forebody lip suction loss, boattail pressure, and skin friction affect the design of nacelles for high bypass ratio, short duct engines. The mutual relationship of the fan nozzle, hot gas nozzle, the gas generator cowling, and the fan cowl is discussed.

SAE MOBILUS

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

Access SAE MOBILUS »

Preview Document Add to Cart
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

Aerodynamic Considerations for Engine Exhaust Design for Subsonic High Bypass Fan Engines

660734

View Details

TECHNICAL PAPER

Atomization of a Liquid Jet Under Swirling Air Stream

982612

View Details

TECHNICAL PAPER

An Analytical Study of the Effects of Turbine Variable Geometry Operation on Turbine Blade Cooling Requirements for Fixed Match Point Turbojet Application

760916

View Details

X