Design And Experimental Results For A Natural Laminar Flow Airfoil For General Aviation Application
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Design And Experimental Results For A Natural Laminar Flow Airfoil For General Aviation Application
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Author : Dan M. Somers
language : en
Publisher:
Release Date : 1981
Design And Experimental Results For A Natural Laminar Flow Airfoil For General Aviation Application written by Dan M. Somers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Aerofoils categories.
A natural-laminar-flow airfoil for general aviation applications, the NLF(1)-0416, was designed and analyzed theoretically and verified experimentally in the Langley Low-Turbulence Pressure Tunnel. The basic objective of combining the high maximum lift of the NASA low-speed airfoils with the low cruise drag of the NACA 6-series airfoils was achieved. The safety requirement that the maximum lift coefficient not be significantly affected with transition fixed near the leading edge was also met. Comparisons of the theoretical and experimental results show excellent agreement. Comparisons with other airfoils, both laminar flow and turbulent flow, confirm the achievement of the basic objective.
Design And Experimental Results For A Flapped Natural Laminar Flow Airfoil For General Aviation Applications
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Author : Dan M. Somers
language : en
Publisher:
Release Date : 1981
Design And Experimental Results For A Flapped Natural Laminar Flow Airfoil For General Aviation Applications written by Dan M. Somers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Aerofoils categories.
A flapped natural laminar flow airfoil for general aviation applications, the NLF(1)-0215F, has been designed and analyzed theoretically and verified experimentally in the Langley Low Turbulence Pressure Tunnel. The basic objective of combining the high maximum lift of the NASA low speed airfoils with the low cruise drag of the NACA 6 series airfoils has been achieved. The safety requirement that the maximum lift coefficient not be significantly affected with transition fixed near the leading edge has also been met. Comparisons of the theoretical and experimental results show generally good agreement.
Design And Experimental Results For A Natural Laminar Flow Airfoil For General Aviation Applications
DOWNLOAD
Author : Dan M. Somers
language : en
Publisher:
Release Date : 1981
Design And Experimental Results For A Natural Laminar Flow Airfoil For General Aviation Applications written by Dan M. Somers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with categories.
Airfoil Design And Data
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Author : Richard Eppler
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
Airfoil Design And Data written by Richard Eppler and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Technology & Engineering categories.
This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.
Laminar Flow Aircraft Certification
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Author :
language : en
Publisher:
Release Date : 1986
Laminar Flow Aircraft Certification written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Fluid dynamics categories.
Experimental Results For A Flapped Natural Laminar Flow Airfoil With High Lift Drag Ratio
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Author :
language : en
Publisher:
Release Date : 1984
Experimental Results For A Flapped Natural Laminar Flow Airfoil With High Lift Drag Ratio written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Aerofoils categories.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1987
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Science categories.
Natural Laminar Flow Airfoil Design Considerations For Winglets On Low Speed Airplanes
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Author : Cornelis P. Van Dam
language : en
Publisher:
Release Date : 1984
Natural Laminar Flow Airfoil Design Considerations For Winglets On Low Speed Airplanes written by Cornelis P. Van Dam and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Airplanes categories.
Natural Laminar Flow Airfoil Design Considerations For Winglets On Low Speed Airplanes
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Author : C. P. Vandam
language : en
Publisher:
Release Date : 1984
Natural Laminar Flow Airfoil Design Considerations For Winglets On Low Speed Airplanes written by C. P. Vandam and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with categories.
Winglet airfoil section characteristics which significantly influence cruise performance and handling qualities of an airplane are discussed. A good winglet design requires an airfoil section with a low cruise drag coefficient, a high maximum lift coefficient, and a gradual and steady movement of the boundary layer transition location with angle of attack. The first design requirement provides a low crossover lift coefficient of airplane drag polars with winglets off and on. The other requirements prevent nonlinear changes in airplane lateral/directional stability and control characteristics. These requirements are considered in the design of a natural laminar flow airfoil section for winglet applications and chord Reynolds number of 1 to 4 million.
Natural Laminar Flow And Laminar Flow Control
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Author : R. W. Barnwell
language : en
Publisher:
Release Date : 1992
Natural Laminar Flow And Laminar Flow Control written by R. W. Barnwell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Science categories.