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INCORPORATING THE INSTITUTION OF AERONAUTICAL ENGINEERS AND THE HELICOPTER ASSOCIATION OF GREAT BRITAIN
HOBBS J D
Helicopters Investigation into the optimum use of advanced displays in future
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achieved acoustic aero aerodynamic Aerospace air transport aircraft noise airframe airline airport airworthiness AMRAeS analysis anechoic chamber angle Aviation British Airways bypass ratio CEng Chairman components compressor Concorde configuration craft cruise display drag duct dynamic effect efficiency engine equations equipment ESDU facility factor Figure flight flow flying FRAeS frequency fuel gas turbine helicopter icing Illustrated improved increase indicator industry installation instruments load London Mach number measure ment method MRAeS NASA TN navigation nozzle nutation ONERA TP operating costs overall paper parameters passenger payload performance pilot Politecnico di Torino possible President pressure problems production programme range reduced Rolls-Royce rotor Royal Aeronautical Society Royal Air Force Secretary shown in Fig shows spacecraft Spacelab speed standards structure subsonic supersonic surface take-off thrust tion turbine turbofan velocity weight wing