Series of Articles on Compressor and Fan Design Written by German Engineers: The influence of physical dimensions ... and flow conditions ... on compressor characteristics

Series of Articles on Compressor and Fan Design Written by German Engineers: The influence of physical dimensions ... and flow conditions ... on compressor characteristics
Author: United States. Navy Dept. Bureau of Ships
Publisher:
Total Pages: 194
Release: 1946
Genre: Air-compressors
ISBN:

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Jet Web

Jet Web
Author: Dietrich Eckardt
Publisher: Springer Nature
Total Pages: 748
Release: 2023-02-03
Genre: Technology & Engineering
ISBN: 3658385316

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The present book describes the development history of turbojet engines, mainly in the web-type triangle Great Britain (USA) - Germany - Switzerland from early beginnings in the 1920s up to the first practical usage in the 1950s, before the still unbroken, grand impact of aero propulsion technology on global air traffic started. interconnections are highlighted, including the considerable impact of axial-flow compressor design know-how of the Swiss/German company BBC Brown Boveri & Cie. on both sides. The author reveals significant undercurrents which led to a considerable exchange, and thus change in understanding of the technical-historical perspective, especially in the decisive years before WWII, and thus closes gaps in the unilateral views of this ground-breaking technical advancement. The old ‘Whittle vs. von Ohain Saga’ is not repeated in full, but addressed in sufficient detail to understand the considerably enlarged narrative scope.

Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine

Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine
Author: Arthur M. Trout
Publisher:
Total Pages: 608
Release: 1950
Genre: Airplanes
ISBN:

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Charts are presented by means of which the jet pressure ratio that give optimum division of power between propeller and jet for maximum total thrust power may be determined for any turbine-propeller engine with or without intercooling, reheat, regeneration, or any combination of these modifications.