The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
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Page 632
... RANGE GEOPOTENTIAL ALTITUDE , 1000 FEET 320 280 range . 240 .200 UPPER LIMIT ( LIFT ) 160 120 1.8 80 40 LOWER LIMIT ( HEATING ) T L O 2 4 6 8 10 12 14 16 18 20 Figure 5. Corridor of flight . 1.6 MXIX L / D XI / CRF 1.4 4 12 00 1.0 0.8 6 ...
... RANGE GEOPOTENTIAL ALTITUDE , 1000 FEET 320 280 range . 240 .200 UPPER LIMIT ( LIFT ) 160 120 1.8 80 40 LOWER LIMIT ( HEATING ) T L O 2 4 6 8 10 12 14 16 18 20 Figure 5. Corridor of flight . 1.6 MXIX L / D XI / CRF 1.4 4 12 00 1.0 0.8 6 ...
Page 639
... range . Reduced range permits seating of up to twelve passengers . The removal of passenger seats results in a cargo capacity of some 265 cu ft ( 7-6 m3 ) . A great variety of goods weighing up to 1390 lb ( 630 kg ) , may be transported ...
... range . Reduced range permits seating of up to twelve passengers . The removal of passenger seats results in a cargo capacity of some 265 cu ft ( 7-6 m3 ) . A great variety of goods weighing up to 1390 lb ( 630 kg ) , may be transported ...
Page 936
... range operations . Figure 3 shows the Range / Payload capability of the Trident 1E , 2 , 3 , and 3B , compared with the Trident 1 as it entered service in 1964. Also shown is the design point for the Trident 1 . The objectives on the ...
... range operations . Figure 3 shows the Range / Payload capability of the Trident 1E , 2 , 3 , and 3B , compared with the Trident 1 as it entered service in 1964. Also shown is the design point for the Trident 1 . The objectives on the ...
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Aero aerodynamic aerofoil Aeronautical Journal aeroplane air transport airline airport angle application associated Aviation blade boundary layer British BRITISH AIRCRAFT CORPORATION cargo CEng civil Civil Air Transport configuration conventional cost cross-coupling dynamic effect engine equipment fibres field Figure flight flow flying FRAeS fuselage future Harrier Hawker Siddeley Aviation helicopter hover Illustrated increase industry lecture lift lift-fan London Mach number man-powered flight mechanical ment methods military NASA TN noise level obtained operation organisation outer space paper passengers performance pilot plate polymers possible present problem programme propulsion ratio rotorcraft Royal Aeronautical Society Royal Air Force satellite shown in Fig speed STOL structure Sud Aviation supersonic tail rotor take-off technical techniques Technology temperature thrust tion traffic turbine V/STOL vector vehicle velocity VTOL weight Westland wing