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Conceptual design of single turbofan engine powered light aircraft (1977)

Voorhees, C. G. ; Snyder, F. S. ; Heinrich, A. M. ; [et al.]

In: CASI

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Publication Date: 2019-06-27

Description: 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.

Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE

Type: NASA-CR-151972

Format: application/pdf

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