Fighter aircraft dealt with whose normal duty would be to 'stand off' at modest flight speeds and achieve high supersonic speeds only during combat; arrangement where heat is retained in 'pipe line' until fuel is discharged to engine, not allowing any fuel to return to low pressure zones; suitability of two-circuit spill system as heat sink for supply of fuel directly to combustion chamber; effect of fuel temperature on gas turbine control systems.
Fuel systems and high speed flight
Shell Aviation News
Shell Aviation News ; n 233
1957
5 pages
Aufsatz (Zeitschrift)
Englisch
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High speed flight propulsion systems
TIBKAT | 1991
|AIAA | 1996
|SLUB | 1956
|Wiley | 2010
|Engineering Index Backfile | 1947
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