The Aerodynamic Design Of Wings With Cambered Span Having Minimum Induced Drag
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The Aerodynamic Design Of Wings With Cambered Span Having Minimum Induced Drag
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Author : Clarence D. Cone (Jr.)
language : en
Publisher:
Release Date : 1963
The Aerodynamic Design Of Wings With Cambered Span Having Minimum Induced Drag written by Clarence D. Cone (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Airplanes categories.
"The basic aerodynamic relations needed for the design of wings with cambered span having a minimum induced drag at specified flight conditions are developed for wings of arbitrary spanwise camber. Procedures are also developed for determining the physical wing form required to obtain the maximum value of lift-drag ratio at cruise, when the wing spanwise camber-line and section profiles are specified, by optimizing the wing chord and twist distributions with respect to both profile and induced drags. The application of the design procedure is illustrated by determining the physical wing form for a circular-arc spanwise camber line. The efficiency of this cambered wing is compared with that of an equal-span, flat wing of elliptical planform which satisfies the same set of fright operating conditions as does the cambered wing. The wing pitching- moment equations for optimally loaded cambered-span wings at design flight conditions are also developed for use in trim analyses on complete aircraft designs."--Page 1.
The Aerodynamic Design Of Wings With Cambered Span Having Minimum Induced Drag
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Author : Clarence D. Cone (Jr.)
language : en
Publisher:
Release Date : 1963
The Aerodynamic Design Of Wings With Cambered Span Having Minimum Induced Drag written by Clarence D. Cone (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Airplanes categories.
"The basic aerodynamic relations needed for the design of wings with cambered span having a minimum induced drag at specified flight conditions are developed for wings of arbitrary spanwise camber. Procedures are also developed for determining the physical wing form required to obtain the maximum value of lift-drag ratio at cruise, when the wing spanwise camber-line and section profiles are specified, by optimizing the wing chord and twist distributions with respect to both profile and induced drags. The application of the design procedure is illustrated by determining the physical wing form for a circular-arc spanwise camber line. The efficiency of this cambered wing is compared with that of an equal-span, flat wing of elliptical planform which satisfies the same set of fright operating conditions as does the cambered wing. The wing pitching- moment equations for optimally loaded cambered-span wings at design flight conditions are also developed for use in trim analyses on complete aircraft designs."--Page 1.
Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1963
Nasa Technical 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 1963 with Aerodynamics categories.
The Spanwise Distribution Of Lift For Minimum Induced Drag Of Wings Having A Given Lift And A Given Bending Moment
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Author : Robert T. Jones
language : en
Publisher:
Release Date : 1950
The Spanwise Distribution Of Lift For Minimum Induced Drag Of Wings Having A Given Lift And A Given Bending Moment written by Robert T. Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Airplanes categories.
The problem of the minimum induced drag of wings having a given lift and a given span is extended to include cases in which the bending moment to be supported by the wing is also given. Expressions for the spanwise load distribution and the minimum drag in terms of the lateral position of the load centroid are given. The results show a 15-percent reduction of the induced drag with a 15-percent increase in span over that for an elliptic loading having the same total lift and bending moment.
The Bending Moment Distribution Of Chambered Span Wing Systems Having Minimum Induced Drag
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Author : Clarence D. Cone
language : en
Publisher:
Release Date : 1963
The Bending Moment Distribution Of Chambered Span Wing Systems Having Minimum Induced Drag written by Clarence D. Cone and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Airplanes categories.
Applied Wing Theory
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Author : Elliott Gray Reid
language : en
Publisher:
Release Date : 1932
Applied Wing Theory written by Elliott Gray Reid and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1932 with Aerodynamics categories.
The Design Of Sailplanes For Optimum Thermal Soaring Performance
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Author : Clarence D. Cone (Jr.)
language : en
Publisher:
Release Date : 1964
The Design Of Sailplanes For Optimum Thermal Soaring Performance written by Clarence D. Cone (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Atmospheric temperature categories.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1963
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Mechanics, Applied categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1963
Nasa 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 1963 with Aeronautics categories.
Investigation Of Three Tapered 45 Sweptback Cambered And Twisted Wings Covering A Simultaneous Variation In Aspect Ratio And Thickness Ratio And Of One Related Symmetrical Wing At Transonic Speeds By The Wing Flow Method
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Author : Harold I. Johnson
language : en
Publisher:
Release Date : 1953
Investigation Of Three Tapered 45 Sweptback Cambered And Twisted Wings Covering A Simultaneous Variation In Aspect Ratio And Thickness Ratio And Of One Related Symmetrical Wing At Transonic Speeds By The Wing Flow Method written by Harold I. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.