Application of Advanced Methods to Design Loads Determination for the L-1011 Transport-Reference-Cited by-同舟云学术

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

Published:1973-08 Issue:8 Volume:10 Page:449-458
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Stauffer Warren A.¹,Lewolt John G.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/10.2514/3.60248

Reference11 articles.

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

2. Watkins, 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.

3. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

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