Topics covered are: (1) numerical calculation of linearized subsonic flows around wings; (2) procedure for calculating the transonic field of convergent ejectors having the shape of truncated cone bodies of revolution, (3) comparative study of two protection methods for super alloys, i.e. the case of NiAl-type coatings on 1N-100 alloys; (4) explicit form of the optimal piloting law for a rigid aircraft flying in a turbulent atmosphere; (5) evaluation of the stress intensity factor by direct measurements on a loaded cracked structure; and (6) influence of sloshing in wing tip tanks on the natural vibration modes of an aircraft.
La Recherche Aerospatiale. Bimonthly Bulletin No. 1974-5
1975
171 pages
Report
No indication
English
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