Authors
John F Gundlach IV, Philippe-Andre Tetrault, Frank H Gern, Amir H Nagshineh-Pour, Andy Ko, Joseph A Schetz, William H Mason, Rakesh K Kapania, William H Mason, Bernard Grossman, Raphael T Haftka
Publication date
2000/11
Journal
Journal of aircraft
Volume
37
Issue
6
Pages
976-983
Description
T/W= aircraft thrust-to-weightratio t/c= thickness-to-chordratio W f= aircraft weight at the end of the cruise leg Wi= aircraft weight at initial cruise YE= spanwise distance to engine, ft c 2= second segment climb gradient j a= airfoil technology factor K= wing sweep angle at quarter chord
Total citations
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