Horizontal Tail Loads-Reference-Cited by-同舟云学术

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Horizontal Tail Loads

Published:1996-01-01 Issue: Volume: Page:115-142
ISSN:
Container-title:Structural Loads Analysis for Commercial Transport Aircraft
language:
Short-container-title:

Author:

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600862465.0115.0142

Reference6 articles.

1. 'Anon. "Part 25-Airworthiness Standards: Transport Category Airplanes," Federal Aviation Regulations, U.S. Dept. of Transportation,Jan.1994.

2. 2Anon."Part 4b-AirplaneAirworthiness:TransportCategories,"CivilAirRegulations, Civil AeronauticsBoard, Dec.1953.

3. 3Pratt, K. G., and Walker, W. G. "Revised Gust Load Formula and a Re-Evaluation of V-GDataTakenonCivilTransportAirplanesfrom 1933 to 1950,"NACARept. 1206,Sept. 1953.

4. 'Anon. "Part 25-Airworthiness Standards: Transport Category Airplanes," Federal Aviation Regulations, U.S. Dept. of Transportation,Jan.1994.

5. 2Anon."Part 4b-AirplaneAirworthiness:TransportCategories,"CivilAirRegulations, Civil AeronauticsBoard, Dec.1953.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Wind Tunnel Testing of an Aeroelastically Tailored Horizontal Stabilizer;AIAA SCITECH 2023 Forum;2023-01-19

2. Improving Horizontal Stabilizer Performance Using Aeroelastic Tailoring;AIAA SCITECH 2022 Forum;2022-01-03

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