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.
An Investigation of the Aerodynamics and Cooling of a Horizontally-Opposed Engine Installation
SAE Business Aircraft Meeting, Century 2 ; 1977 ; Wichita, KS, United States
01.01.1977
Aufsatz (Konferenz)
Keine Angabe
Englisch
An Investigation of the Aerodynamics and Cooling of a Horizontally-Opposed Engine Installation
SAE Technical Papers | 1977
|Determination of Cooling Air Mass Flow for a Horizontally - Opposed Aircraft Engine Installation#
SAE Technical Papers | 1979
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