The conceptual design of a four place single turbofan engine powered light aircraft was accomplished utilizing contemporary light aircraft conventional design techniques as a means of evaluating the NASA-Ames General Aviation Synthesis Program (GASP) as a preliminary design tool. In certain areas, disagreement or exclusion were found to exist between the results of the conventional design and GASP processes. Detail discussion of these points along with the associated contemporary design methodology are presented.
Conceptual Design of Single Turbofan Engine Powered Light Aircraft
1977
174 pages
Report
No indication
English
RECENT CONCEPTUAL DESIGN STUDIES OF SINGLE TURBOFAN ENGINE AIRCRAFT
SAE Technical Papers | 1977
|Summary of Systems Design Studies of Turbofan Powered Light Aircraft
SAE Technical Papers | 1975
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