Browse Publications Technical Papers 770467
1977-02-01

An Investigation of the Aerodynamics and Cooling of a Horizontally-Opposed Engine Installation 770467

A research program to investigate the aerodynamics of reciprocating aircraft engine cooling installations is discussed. Current results from a flight test program are presented concerning installation flow measurement methods. The influence of different inlet designs on installation cooling effectiveness and efficiency are described.

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

Determination of Cooling Air Mass Flow for a Horizontally - Opposed Aircraft Engine Installation#

790609

View Details

TECHNICAL PAPER

The Development of Reciprocating Engine Installation Data for General Aviation Aircraft

730325

View Details

TECHNICAL PAPER

Full-Scale Study of the Cooling System Aerodynamics of an Operating Piston Engine Installed in a Light Aircraft Wing Panel

810623

View Details

X