The Aeronautical Journal, Volume 73Royal Aeronautical Society, 1969 - Aeronautics |
From inside the book
Results 1-3 of 86
Page 773
Ground attack aircraft . Take - off weight Figure 9. Fuel weight ratio . ( after P. Lloyd : Journ . R.Ae.S. Feb. 1968 ) Figure 11. Powerplant specific weight . HUNTER STRUCTURE POWER UNIT 20 % Figure 12. Comparative take - off weight ...
Ground attack aircraft . Take - off weight Figure 9. Fuel weight ratio . ( after P. Lloyd : Journ . R.Ae.S. Feb. 1968 ) Figure 11. Powerplant specific weight . HUNTER STRUCTURE POWER UNIT 20 % Figure 12. Comparative take - off weight ...
Page 939
... weight reduction campaigns , resulting in a saving of approximately 700 lb ( 317 kg ) between the Trident 1 and 1E ... weight and cost . Efforts were also made , to reduce manufacturing LIFT COEFFICIENT 57 TRACK FLAPS DOWN- UNDERNEATH ...
... weight reduction campaigns , resulting in a saving of approximately 700 lb ( 317 kg ) between the Trident 1 and 1E ... weight and cost . Efforts were also made , to reduce manufacturing LIFT COEFFICIENT 57 TRACK FLAPS DOWN- UNDERNEATH ...
Page 947
... weight reduction campaigns , resulting in a saving of approximately 700 lb ( 317 kg ) between the Trident 1 and 1E ... weight and cost . Efforts were also made , to reduce manufacturing LIFT COEFFICIENT C TRACK FLAPS DOWN UNDERNEATH ...
... weight reduction campaigns , resulting in a saving of approximately 700 lb ( 317 kg ) between the Trident 1 and 1E ... weight and cost . Efforts were also made , to reduce manufacturing LIFT COEFFICIENT C TRACK FLAPS DOWN UNDERNEATH ...
Other editions - View all
Common terms and phrases
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