Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 2.0, and 2.8

Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 2.0, and 2.8 PDF Author: Richard H. Cavicchi
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ISBN:
Category : Aeronautics
Languages : en
Pages : 54

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Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 2.0, and 2.8

Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 2.0, and 2.8 PDF Author: Richard H. Cavicchi
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 54

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Analysis of Limitations Imposed on One-spool Turboprop-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8

Analysis of Limitations Imposed on One-spool Turboprop-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8 PDF Author: Richard H. Cavicchi
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ISBN:
Category : Airplanes
Languages : en
Pages : 66

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Analysis of Limitations Imposed on One-spool Ducted-fan-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8

Analysis of Limitations Imposed on One-spool Ducted-fan-engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8 PDF Author: Richard H. Cavicchi
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ISBN:
Category :
Languages : en
Pages : 47

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Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers

Analysis of Limitations Imposed on One-spool Turbojet-engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers PDF Author: Richard H. Cavicchi
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ISBN:
Category :
Languages : en
Pages : 49

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Design Analysis of a Subsonic Nuclear-powered Logistic Airplane with Helium-cooled Reactor

Design Analysis of a Subsonic Nuclear-powered Logistic Airplane with Helium-cooled Reactor PDF Author:
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Category : Nuclear aircraft
Languages : en
Pages : 258

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Aerodynamic Design of Axial-flow Compressors

Aerodynamic Design of Axial-flow Compressors PDF Author: Lewis Research Center
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ISBN:
Category : Axial flow compressors
Languages : en
Pages : 542

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 860

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Aerodynamic Design of Axial Flow Compressors

Aerodynamic Design of Axial Flow Compressors PDF Author: Robert O. Bullock
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Category : Axial flow compressors
Languages : en
Pages : 552

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
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Category : Military art and science
Languages : en
Pages : 1746

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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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ISBN:
Category :
Languages : en
Pages : 208

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