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Design and Analysis of a Telescopic Wing
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English
Abstract
Unique in the era of fail-safe aircraft design is the two-spar telescopic wing. This paper examines the structural integrity of this wing for use on the Advanced Flying Automobile as described in the “Design Concepts and Market Opportunities for Flying Automobiles”, Reference 1.
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Citation
Czajkowski, M., "Design and Analysis of a Telescopic Wing," SAE Technical Paper 932605, 1993, https://doi.org/10.4271/932605.Also In
References
- Sarh B. “Design Concepts and Market Opportunities for “Flying Automobiles”” SAE Paper 921570
- Sarh B. “Telescopic Wing” United State Patent, No. 4,824,053 Apr. 25 1989
- Peterson R.E. “Stress Concentration Factors” John Wiley & Sons, Inc. 1974
- Faupel J. H. “Engineering Design” A Wiley-Interscience Publication Second 1981
- Kleinlogel A. “Rigid Frame Formulas” Fredrick Ungar Publishing Co. Second 1973
- HEXCEL “Design Handbook for Honeycomb Sandwich Structures” October 1967
- Roark R.J. “Formulas for Stress and Strain” Fifth 1975
- Harris T.A. “Rolling Bearing Analysis” John Wiley & Sons Inc. 1966