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Structural Airworthiness of New and Aging Aircraft: Load Spectra Derivation and Measurement
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English
Abstract
This paper provides an overview of various analytical load spectra methods and compares analytical and measured data.
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Authors
Citation
Smith, J., "Structural Airworthiness of New and Aging Aircraft: Load Spectra Derivation and Measurement," SAE Technical Paper 931257, 1993, https://doi.org/10.4271/931257.Also In
References
- “Fatigue Evaluation of Wing and Associated Structure on Small Airplanes.” May 1973
- Sewell R. T. “Analysis of Flight Loads During Low-Altitude Pipeline Patrol Operations.” December 1968
- “Average Gust Frequencies Subsonic Transport Aircraft.” Engineering Sciences Data Item No. 69023 May 1972
- Jewel, Joseph W. Jr. “Progress Report on the NASA V-G/VGH General Aviation Program.” May 4 1971
- Hoblit Frederic M. “Gust Loads on Aircraft: Concepts and Applications.” AIAA Education Series 1988