Knock Limited Performance Tests Of 2 2 3 4 Tetramethylpentane 2 3 3 4 Tetramethylpentane 3 4 4 Trimethyl 2 Pentene And 2 3 4 Trimethyl 2 Pentene In Small Scale And Full Scale Cylinders
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Knock Limited Performance Tests Of 2 2 3 4 Tetramethylpentane 2 3 3 4 Tetramethylpentane 3 4 4 Trimethyl 2 Pentene And 2 3 4 Trimethyl 2 Pentene In Small Scale And Full Scale Cylinders
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Author : Edmund R. Jonash
language : en
Publisher:
Release Date : 1946
Knock Limited Performance Tests Of 2 2 3 4 Tetramethylpentane 2 3 3 4 Tetramethylpentane 3 4 4 Trimethyl 2 Pentene And 2 3 4 Trimethyl 2 Pentene In Small Scale And Full Scale Cylinders written by Edmund R. Jonash and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Airplanes categories.
Knock-limited tests were conducted with F-4, F-3, and 17.6 small-scale engines and with a full-scale cylinder on blends containing the following purified hydrocarbons: 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene.
Wartime Report
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Author :
language : en
Publisher:
Release Date : 194?
Wartime Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 194? with Aeronautics categories.
Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Wartime Report E
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
Wartime Report E written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Airplanes categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1949
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.
Knock Limited Performance Of Several Branched Paraffins And Olefins
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Author : R. S. Genco
language : en
Publisher:
Release Date : 1948
Knock Limited Performance Of Several Branched Paraffins And Olefins written by R. S. Genco and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Alkanes categories.
At mild or moderate engine severity, 2,2,3,3-tetramethylpentane blend was highest in knock limit of the paraffins tested, but at severe conditions it was lowest; at severe (F-3) conditions, triptane blend was best.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1949
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.
Bibliography Of Scientific And Industrial Reports
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Author :
language : en
Publisher:
Release Date : 1948
Bibliography Of Scientific And Industrial Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Science categories.
Velocity Distribution On Wing Sections Of Arbitrary Shape In Compressible Potential Flow
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Author : Lipman Bers
language : en
Publisher:
Release Date : 1950
Velocity Distribution On Wing Sections Of Arbitrary Shape In Compressible Potential Flow written by Lipman Bers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerofoils categories.
The method of computing velocity and pressure distributions along wing profiles under the assumption of the simplified density-speed relation, outlined in NACA Technical Note 1006, is extended to the case of a nonsymmetrical profile and a flow with circulation. The shape of the profile, the speed of the undisturbed flow, and a parameter determing the angle of attack may be prescribed. The problem is reduced to a nonlinear integral equation which can be solved numerical by an iteration method. A numerical example is given.
Technical Note
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Author :
language : en
Publisher:
Release Date : 1948
Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aeronautics categories.