The Bending Moment Distribution Of Chambered Span Wing Systems Having Minimum Induced Drag PDF Download
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Author | : Clarence D. Cone |
Publisher | : |
Total Pages | : 40 |
Release | : 1963 |
Genre | : Airplanes |
ISBN | : |
Download The Bending-moment Distribution of Chambered-span Wing Systems Having Minimum Induced Drag Book in PDF, ePub and Kindle
Author | : Robert T. Jones |
Publisher | : |
Total Pages | : 708 |
Release | : 1950 |
Genre | : Airplanes |
ISBN | : |
Download The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment Book in PDF, ePub and Kindle
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.
Author | : United States. Department of Commerce. Office of Technical Services |
Publisher | : |
Total Pages | : 618 |
Release | : 1963 |
Genre | : Government publications |
ISBN | : |
Download Keywords Index to U.S. Government Technical Reports (permuted Title Index). Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 92 |
Release | : 1963-07 |
Genre | : Government publications |
ISBN | : |
Download Keywords Index to U.S. Government Technical Reports Book in PDF, ePub and Kindle
Author | : Clarence D. Cone (Jr.) |
Publisher | : |
Total Pages | : 36 |
Release | : 1963 |
Genre | : Airplanes |
ISBN | : |
Download The Aerodynamic Design of Wings with Cambered Span Having Minimum Induced Drag Book in PDF, ePub and Kindle
"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.
Author | : Hans-Jörg Bullinger |
Publisher | : Springer Science & Business Media |
Total Pages | : 560 |
Release | : 2009-05-10 |
Genre | : Technology & Engineering |
ISBN | : 3540885463 |
Download Technology Guide Book in PDF, ePub and Kindle
Use this technology guide to find descriptions of today’s most essential global technologies. Clearly structured and simply explained, the book’s reference format invites even the casual reader to explore the stimulating innovative ideas it contains.
Author | : Clarence D. Cone (Jr.) |
Publisher | : |
Total Pages | : 0 |
Release | : 1963 |
Genre | : Airplanes |
ISBN | : |
Download The Aerodynamic Design of Wings with Cambered Span Having Minimum Induced Drag Book in PDF, ePub and Kindle
"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.
Author | : New York Public Library. Economic and Public Affairs Division |
Publisher | : |
Total Pages | : 794 |
Release | : 1972 |
Genre | : Government publications |
ISBN | : |
Download Catalog of Government Publications in the Research Libraries Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 726 |
Release | : 1984 |
Genre | : Technology & Engineering |
ISBN | : |
Download The Software Catalog Book in PDF, ePub and Kindle
Author | : MENU Staff |
Publisher | : Elsevier Science & Technology |
Total Pages | : 726 |
Release | : 1987 |
Genre | : Science |
ISBN | : |
Download The Software Catalog Book in PDF, ePub and Kindle