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Author : S. Kirkby
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (977 download)
Download or read book Wing Body Interference at Supersonic Speeds written by S. Kirkby and published by . This book was released on 1947 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jack N. Nielsen
Publisher :
ISBN 13 :
Total Pages : 63 pages
Book Rating : 4.:/5 (249 download)
Download or read book Wing-body Interference at Supersonic Speeds with an Application to Combinations with Rectangular Wings written by Jack N. Nielsen and published by . This book was released on 1952 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt: An exact theoretical method is developed that permits the determination of the pressure field of a wing-body combination having a circular body and wings with supersonic leading and trailing edges. Detailed calculations are performed for the case of a rectangular wing or all-movable control surface on a body at zero angle of attack. Design charts are presented showing the effect of interference on the lift and center-of-pressure position of the wings. The physical basis of the interference is discussed.
Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (464 download)
Download or read book Interference Between Wing and Body at Supersonic Speeds: Data report, pressure distribution tests of wing-body interference models at Mach no. of 2.0, phase V tests of August 1951 written by and published by . This book was released on 1947 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Erik Larson
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (11 download)
Download or read book Wing-body Interference at Moderate Supersonic Speeds. A Comparison Between Panel Method and Experiment written by Erik Larson and published by . This book was released on 1976 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. C. MEYER
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book Favorable Wing-body Interference for Aircraft at Supersonic Speed: an Analytic Study of Design Parameters written by R. C. MEYER and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jack N. Nielsen
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (258 download)
Download or read book Quasi-cylindrical Theory of Wing Body Interference at Supersonic Speeds and Comparison with Experiment written by Jack N. Nielsen and published by . This book was released on 1955 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harry Edward Bailey
Publisher :
ISBN 13 :
Total Pages : 264 pages
Book Rating : 4.3/5 (91 download)
Download or read book WING-BODY INTERFERENCE AT SUPERSONIC SPEEDS. written by Harry Edward Bailey and published by . This book was released on 1954 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jack N. Nielsen
Publisher :
ISBN 13 :
Total Pages : 43 pages
Book Rating : 4.:/5 (11 download)
Download or read book Method for Estimating Lift Interference of Wing-body Combinations at Supersonic Speeds written by Jack N. Nielsen and published by . This book was released on 1951 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. M. Pritulo
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Favorable Interference of Optimized Wing-body Combination with Inlets at Supersonic Speed written by T. M. Pritulo and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Henry H. Tompkins
Publisher :
ISBN 13 :
Total Pages : 81 pages
Book Rating : 4.:/5 (115 download)
Download or read book A Calculation of Interference Effects at Supersonic Speed for Two Wing-body Configurations written by Henry H. Tompkins and published by . This book was released on 1952 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Carlo Ferrari
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (464 download)
Download or read book Interference Between Wing and Body at Supersonic Speeds written by Carlo Ferrari and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ralph L. Carmichael
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Integrated Approach to the Analysis and Design of Wings and Wing-body Combinations in Supersonic Flow written by Ralph L. Carmichael and published by . This book was released on 1966 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Carlo Ferrari
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (977 download)
Download or read book Interference Between Wing and Body at Supersonic Speeds written by Carlo Ferrari and published by . This book was released on 1948 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aeronautical Research Council
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (31 download)
Download or read book Interference on a Wing Due to a Body at Supersonic Speeds written by Aeronautical Research Council and published by . This book was released on 1952 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : S. Kirkby
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Interference on a Wing Due to a Body at Supersonic Speeds written by S. Kirkby and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Goetz H. Klopfer
Publisher :
ISBN 13 :
Total Pages : 87 pages
Book Rating : 4.:/5 (227 download)
Download or read book Basic Studies of Wing-Body Interference at High Angles of Attack and Supersonic Speeds written by Goetz H. Klopfer and published by . This book was released on 1979 with total page 87 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of computing the steady inviscid supersonic flows about thin wings having sharp subsonic leading edges and leading-edge separation is solved in this paper. Both wings alone or wings in the presence of the body are considered. To obtain an efficient procedure the steady Euler equations are used as the basic governing equations as opposed to the more complicated Navier-Stokes equation. The viscous effects, important near the sharp leading edges, are simulated by a Kutta condition applied at the leading edges of the wings. The rest of the flow field is essentially controlled by the inviscid equations. The equations, written in conservation form in generalized curvilinear coordinates, are approximated by MacCormack's second-order accurate predictor-corrector algorithm. The flow tangency conditions at the body surface are satisfied by Abbett's scheme and the outer bow-shock position by the Rankine-Hugoniot jump relations. Internal shock waves or tangentially discontinuities are captured. The slip surface emanating from the leading edge of the sharp wing excited nonlinear instabilities in the MacCormack's scheme, which were stabilized by special flow dependent fourth-order damping terms.
Author : William C. Pitts
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (67 download)
Download or read book Comparison Between Theory and Experiment for Interference Pressure Field Between Wing and Body at Supersonic Speeds written by William C. Pitts and published by . This book was released on 1954 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution data were obtained for a wing-body combination at Mach numbers of 1.48 and 2.00 and at Reynolds numbers of 600,000, 1,200,000 and 1,500,000 to investigate the effects of wing-body interference. The model was a single-wedge, rectangular wing mounted on a cylindrical body with an ogival nose. The body angle of angle of attack ranged between +6 degrees and -6 degrees and the wing-incidence angle ranged from 0 degrees to -5.7 degrees. The experimental pressure-distribution and span-loading results are compared with the linear, wing-body interference theory of NACA TN 2677.
