An experimental Single Cylinder Test Engine Program is conducted to confirm the analytically projected performance of a two-stroke cycle diesel engine for aircraft applications. Testing confirms the ability of a proposed 4-cylinder version of such an engine to reach the target power at altitude in a highly turbocharged configuration. The experimental program defines all necessary parameters to permit design of a multicylinder engine for eventual flight applications.
Lightweight Two-Stroke Cycle Aircraft Diesel Engine Technology Enablement Program. Volume 3
1985
282 pages
Report
Keine Angabe
Englisch
NASAs rotary engine technology enablement program 1983 trough 1991
Kraftfahrwesen | 1992
|NASA's Rotary Engine Technology Enablement Program -- 1983 Through 1991
SAE Technical Papers | 1992
|