Aluminum structural member component weight as a function of wing loading

Aircraft Design

Volumn 2, Issue 4, 1999, Pages 231-237

  Svoboda, Charlie ^a  

^a University of Kansas   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; STRUCTURAL LOADS;

WING LOADING;

WINGS;

EID: 0033324001     PISSN: 13698869     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1369-8869(99)00019-1     Document Type: Article

References (5)

1. Roskam J. Airplane design, part V: component weight estimation, 1985. Roskam Aviation and Engineering Corporation, 120 East 9th St, Suite 2, Lawrence, KS 66044, (785) 832-0434, FAX (785) 832-0524. http://www.darcorp.com, info@darcorp.com.
2. Taylor JWR. Jane's all the world aircraft. Jane's Publishing Company, 238 City Road, London EC1V 2PU, England, Issues used:1950-1977.
3. Cessna Aircraft Company, P.O. Box 7706, Wichita, KS 67277-7706 (provided 4 three-views not found the other references).
4. Green W. The observer's book of aircraft. Fredrick Warne & Co, LTD., 1961, 1962, 1963, 1967, 1977.
5. Phillips, EH. Beechcraft: pursuit of perfection: a history of beechcraft airplanes. Flying Books, 1992.