Advantages as exemplified in Proteus 3; difficulties experienced in developing Proteus and ingenious, in many cases, simple manner in which these setbacks were overcome; comparison between performance of turboprop and turbojet engine designed to give 1200 lb thrust at 350 mph and 36,000 ft. From paper before Roy Aeronautical Soc. (See also Aeroplane v 84 n 2179 Apr 24 1953 p 540)
Proof of turbo-prop
Flight
Flight ; 63 , n 2311
1953
581 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1955
|Engineering Index Backfile | 1955
|Engineering Index Backfile | 1955
|TURBO PROP CONTROLS - HOW COMPLICATED?
SAE Technical Papers | 1953
|Allison t56 turbo-prop aircraft engine
Engineering Index Backfile | 1955
|