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F Legrand THE NEXT GENERATION OF FRENCH HELICOPTERS
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achieved aerodynamic Aeronautical aircraft airport application associated Aviation become blade British civil compared complete considerable considered conventional cost course detailed direction discussed effect efficiency element engine equipment example experience field Figure flight flow flying forces fuel further future give given Government ground helicopter Illustrated important improved increase indicated industry interest Journal landing lecture lift limited load London major materials means measurements mechanical methods NASA noise obtained operating passengers performance pilot position possible present pressure problems production range ratio reduced reference response roll rotor Royal shown shows Society solution space speed structure temperature thrust tion transport Trident turbine unit V/STOL VTOL weight wing