Name: System Study for Axial Vane Engine Technology
Price: 1067.00 TWD
Availability: InStock
Author: Badley, Patrick R. ; Nasa Technical Reports Server (Ntrs) ; Et Al
ISBN: 9781287236108

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portada System Study for Axial Vane Engine Technology

System Study for Axial Vane Engine Technology

Type

Physical Book

Author

Nasa Technical Reports Server (Ntrs)

Patrick R. Badley

Publisher

Bibliogov

Language

English

Pages

Format

Paperback

Dimensions

24.6 x 18.9 x 0.4 cm

Weight

0.17 kg.

ISBN13

9781287236108

Synopsis "System Study for Axial Vane Engine Technology"

The purpose of this engine feasibility study was to determine the benefits that can be achieved by incorporating positive displacement axial vane compression and expansion stages into high bypass turbofan engines. These positive-displacement stages would replace some or all of the conventional compressor and turbine stages in the turbine engine, but not the fan. The study considered combustion occurring internal to an axial vane component (i.e., Diesel engine replacing the standard turbine engine combustor, burner, and turbine); and external continuous flow combustion with an axial vane compressor and an axial vane turbine replacing conventional compressor and turbine systems.

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System Study for Axial Vane Engine Technology - Badley, Patrick R. ; Nasa Technical Reports Server (Ntrs) ; Et Al

Synopsis "System Study for Axial Vane Engine Technology"

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