The University of Kansas, Flight Research Laboratory is developing an interactive, user-friendly computer program to perform preliminary design and analysis functions for fixed wing airplanes. This paper presents a discussion of the current status of this program. Use of the program is illustrated with an example application to an advanced stealth bomber.
Automated Aircraft Configuration Design and Analysis
Sae Technical Papers
General Aviation Aircraft Meeting and Exposition ; 1989
1989-04-01
Aufsatz (Konferenz)
Englisch
Integration of Configuration Design and Analysis of Aircraft
SAE Technical Papers | 2000
|Configuration Design Analysis of a Prop/Rotor Aircraft
NTIS | 1970
|