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LAND development aircraft D Lockspeiser pp 7074 Feb
ATTITUDE control system for a flexible satellite providing active
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achieved acoustic Aeronautical Air Force aircraft airframe airline airworthiness analysis anechoic application approach aviation CEng Chairman chamber changes civil configuration cost countries direct duct effect efficiency engine equipment example exhaust existing experience facility factor Figure flight flow flying FRAES FRAS frequency fuel further future give given Illustrated important improved increase indicated industry internal landing limited London manufacturer measure ment method MICHIGAN MRAES NASA navigation noise obtained October ONERA TP operating parameters particular performance period pilot possible present President pressure problems production programme range ratio reduced response result roll Royal safety Secretary shown shows sound specific speed standards structure tion transport types units weight wing