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Loading Conditions Measured During Aerobatic Maneuvers
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English
Abstract
A flight test program has been conducted to determine some of the loading conditions experienced in aerobatic maneuvers. A small aerobatic airplane was instrumented to measure three components of linear acceleration, three components of angular velocity, control surface positions, control stick forces, airspeed, and altitude. The magnitude of various loading parameters, singly and in combination, are discussed and used as a basis for assessing some of the structural design requirements for aerobatic category airplanes.
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Authors
Citation
Hall, A., "Loading Conditions Measured During Aerobatic Maneuvers," SAE Technical Paper 700222, 1970, https://doi.org/10.4271/700222.Also In
References
- Jewel, Joseph W. Jr. “Initial Report on Operational Experiences of General Aviation Aircraft.” SAE National Business Aircraft Meeting Wichita, Kansas April 1968
- Federal Aviation Regulations, Part 23-Airworthiness Standards: Normal, Utility, and Acrobatic Category Airplanes
- Mayer John P. Stone, Ralph W. Jr. Hamer Harold A. “Notes on a Large-Scale Statistical Program for the Establishment of Maneuver-Loads Design Criteria for Military Airplanes.” July 1957