Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero PDF Download

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Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero

Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero PDF Author: Willard R. Westphal
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero

Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero PDF Author: Willard R. Westphal
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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Book Description

Experimental Investigation of a Transonic Axial-flow-compressor Rotor Designed for Sonic Velocity with an Inlet Hub-tip Radius Ratio of 0.35

Experimental Investigation of a Transonic Axial-flow-compressor Rotor Designed for Sonic Velocity with an Inlet Hub-tip Radius Ratio of 0.35 PDF Author: Emanuel Boxer
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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Experimental Investigation of a Transonic Axial-flow-compressor Rotor with Double-circular-arc Airfoil Blade Sections

Experimental Investigation of a Transonic Axial-flow-compressor Rotor with Double-circular-arc Airfoil Blade Sections PDF Author: George W. Lewis (Jr.)
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 32

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Experimental Investigation of a 0.35 Hub-Tip Radius Ratio Transonic Axial Flow Rotor Designed for 40 Pounds Per Second Per Square Foot with a Design Tip Diffusion Factor of 0.20

Experimental Investigation of a 0.35 Hub-Tip Radius Ratio Transonic Axial Flow Rotor Designed for 40 Pounds Per Second Per Square Foot with a Design Tip Diffusion Factor of 0.20 PDF Author: Paul T. Yasaki
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1248

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Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43

Blade-element Performance of 0.7 Hub-tip Radius Ratio Axial-flow-pump Rotor with Tip Diffusion Factor of 0.43 PDF Author: James E. Crouse
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 48

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Book Description

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft PDF Author: Clifford J. Moore
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 492

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Book Description
This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990

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Book Description

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety PDF Author: Clifford J. Moore
Publisher:
ISBN:
Category :
Languages : en
Pages : 492

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Book Description

Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1250

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Book Description