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1. Loads applied to the wing
1.1 External loads
The wing of a subsonic transport aircraft has a number of movable surfaces at the leading edge (deployable slats) and trailing edge (flaps and ailerons). The fixed, central structural portion forms the primary wing box (figure 1 ).
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Loads applied to the wing
Root sizing criteria
Bibliography
Bibliography
Websites
CS 25 and FAR 25 certification documents http://easa.europa.eu/document-library/certification-specificationshttp://www.ecfr.gov/cgi-bin/text-idx?c=ecfr&sid=be6ffa6d87343c75e7d49e911c95ab06&rgn=div5&view=text&node=14 :1.0.1.3.11&idno=14
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French Aeronautical and Astronautical Association (3AF) http://www.3af.fr/events
Air and Space Academy (AAE) http://www.academie-air-espace.com/event/newList.php
Institutions
Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO) http://www.isae.fr
École nationale supérieure de mécanique et d'aérotechnique (ISAE-ENSMA) http://www.ensma.fr
Office national d'études et de recherches aérospatiales (ONERA - French...
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