Basis of comparison is engine factor (ratio of engine thrust to weight of propulsion system and payload); maximum speed, rate of climb, maximum altitude, and range determined for each engine as function of aircraft weight; curves show that rocket ramjet and turbojet are superior for high performance short range aircraft; for long range, engines with low specific fuel consumption, like turbofan, produce best overall aircraft.
Comparing aircraft engines by mission requirement and aircraft performance
Aero/Space Eng
Aero/Space Engineering ; 18 , n 1
1959
5 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Fuel And Lubricant Requirement Of Personal Plane Aircraft Engines
SAE Technical Papers | 1950
|SLUB | 1948
|Engineering Index Backfile | 1941
|Engineering Index Backfile | 1940
NTRS | 1977