Knock Limited Performance Of Several Branched Paraffins And Olefins
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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.
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.
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.
Characteristics Of Thin Triangular Wings With Triangular Tip Control Surfaces At Supersonic Speeds With Mach Lines Behind The Leading Edge
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Author : Warren A. Tucker
language : en
Publisher:
Release Date : 1948
Characteristics Of Thin Triangular Wings With Triangular Tip Control Surfaces At Supersonic Speeds With Mach Lines Behind The Leading Edge written by Warren A. Tucker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aerodynamics, Supersonic categories.
A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By restriction to case for which Mach lines from wing apex lie behind the leading edge, a simplified treatment was possible; results of previous work on lift of triangular wings could be used to derive expressions for lift effectiveness, pitching moment, rolling-moment effectiveness, hinge moment due to control deflection, and hinge moment due to angle of attack. Comparisons were made with two-dimensional case.
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.
Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951
Report 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 1951 with Aeronautics categories.
Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1948
Report 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 1948 with Aeronautics categories.
Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951
Annual Report Of The 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 1951 with Aeronautics categories.
List Of Technical Notes 1947 1953
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
List Of Technical Notes 1947 1953 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 1954 with Aeronautics categories.
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.