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Automated Aircraft Configuration Design and Analysis
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English
Abstract
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.
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Citation
Roskam, J. and Malaek, S., "Automated Aircraft Configuration Design and Analysis," SAE Technical Paper 891072, 1989, https://doi.org/10.4271/891072.Also In
References
- Roskam J. Airplane Design, Part I: Preliminary Sizing of Airplanes 1989
- Roskam J. Airplane Design, Part II: Preliminary Configuration Design and Integration of the Propulsion System 1989
- Roskam J. Airplane Design, Part III: Layout Design of Cockpit, Fuselage, Wing and Empennage: Cutaways and inboard Profiles 1989
- Roskam J. Airplane Design, Part IV: Layout Design of Landing Gear and Systems 1989
- Roskam J. Airplane Design, Part V: Component Weight Estimation 1989
- Roskam J. Airplane Design, Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics 1987
- Roskam J. Airplane Design, Part VII: Determination of Stability, Control and Performance Characteristics: FAR and Military Requirements 1988
- Roskam J. Airplane Design, Part VIII: Air plane Cost Estimation: Design, Development, Manufacturing and Operating 1990