Dynamic gust, landing, and taxi loads determination in the design ofthe L-1011.-Reference-Cited by-同舟云学术

Dynamic gust, landing, and taxi loads determination in the design ofthe L-1011.

Published:1973-08 Issue:8 Volume:10 Page:459-467
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Stauffer Warren A.¹,Hoblit Frederic M.¹

Affiliation:

1. Lockheed-California Company, Burbank, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.44383

Reference8 articles.

1. Application of Advanced Methods to Design Loads Determination for the L-1011 Transport

2. 4Watkins, C. E., Woolston, D. S., and Cunningham, H. J. "A Systematic Kernel Function Procedure for Determining Aerodynamic Forces on Oscillating or Steady Finite Wings at Subsonic Speeds," TRR-48,1959, NASA.

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