Method Of Designing Airfoils With Prescribed Velocity Distributions In Compressible Potential Flows

Author : George R. Costello
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.21/5 ( download)

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Download or read book Method of Designing Airfoils with Prescribed Velocity Distributions in Compressible Potential Flows written by George R. Costello and published by . This book was released on 1949 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: By the assumption that the pressure-volume relation is linear, a method is given for computing the airfoil shape with a prescribed velocity distribution in a potential flow of a compressible nonviscous fluid.

Author : John M. Riebs
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.53/5 ( download)

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Download or read book Isolated and Cascade Airfoils with Prescribed Velocity Distribution written by John M. Riebs and published by . This book was released on 1947 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on the suction surface in a given uniform flow of an incompressible perfect liquid is obtained by replacing the boundary of the airfoil by vortices. By this device, a method of solution is developed, which is applicable both to isolated airfoils and to airfoils in cascade. The conformal transformation of the designed airfoil into a circle can then be obtained and the velocity distribution at any angle of attack computed. Numerical illustrations of the method are given for the airfoil in cascade.

Author : George R. Costello
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.19/5 ( download)

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Download or read book Methods of Designing Cascade Blades with Prescribed Velocity Distributions in Compressible Potential Flows written by George R. Costello and published by . This book was released on 1949 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: If the prescribed velocity distribution is not theoretically attainable, the method gives a way of modifying the distribution so as to obtain a blade shape.

Author : Richard Eppler
Publisher : Springer Science & Business Media
ISBN 13 : 3662026465
Total Pages : 569 pages
Book Rating : 4.65/5 ( download)

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Download or read book Airfoil Design and Data written by Richard Eppler and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 569 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 1026 pages
Book Rating : 4.08/5 ( download)

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Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 1026 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Lewis Research Center
Publisher :
ISBN 13 :
Total Pages : 542 pages
Book Rating : 4.01/5 ( download)

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Download or read book Aerodynamic Design of Axial-flow Compressors written by Lewis Research Center and published by . This book was released on 1965 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Hans Hansen
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.81/5 ( download)

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Download or read book Airfoil Design for a Prescribed Velocity Distribution in Transonic Flow by an Integral Method written by Hans Hansen and published by . This book was released on 1975 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 512 pages
Book Rating : 4.12/5 ( download)

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Download or read book Technical Note written by and published by . This book was released on 1951 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Dwight G. Moore
Publisher :
ISBN 13 :
Total Pages : 292 pages
Book Rating : 4.43/5 ( download)

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Download or read book Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section (including Large Temperature Differences and Transpiration Cooling) written by Dwight G. Moore and published by . This book was released on 1953 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : John R. Spreiter
Publisher :
ISBN 13 :
Total Pages : 646 pages
Book Rating : 4.47/5 ( download)

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Download or read book Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds written by John R. Spreiter and published by . This book was released on 1949 with total page 646 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.