Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio

Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio PDF Author: Theodore J. Goldberg
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Category : Airplanes
Languages : en
Pages : 38

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Experimental Investigation of an Axial-flow Supersonic Compressor Having Rounded Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio

Experimental Investigation of an Axial-flow Supersonic Compressor Having Rounded Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio PDF Author: Theodore J. Goldberg
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Category :
Languages : en
Pages : 43

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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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Category : Aeronautics
Languages : en
Pages : 388

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 388

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 716

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Journal of Engineering for Power

Journal of Engineering for Power PDF Author:
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Category : Mechanical engineering
Languages : en
Pages : 578

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Paper

Paper PDF Author:
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Category : Mechanical engineering
Languages : en
Pages : 462

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Advanced Compressors

Advanced Compressors PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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Category : Compressors
Languages : en
Pages : 312

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AGARD Lecture Series

AGARD Lecture Series PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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Category : Aeronautics
Languages : en
Pages :

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Experimental Investigation of the Mixing Loss Behind Trailing Edge of a Cascade of Three 90© Supersonic Turning Passages

Experimental Investigation of the Mixing Loss Behind Trailing Edge of a Cascade of Three 90© Supersonic Turning Passages PDF Author: Luke L. Liccini
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Category : Boundary layer
Languages : en
Pages : 36

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