Author: J. A. BagleyPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Calculated Lift Distribution in Incompressible Flow on Some Sweptback Wings
Author: J. A. BagleyCalculated Lift Distributions in Incompressible Flow on Some Sweptback Wings
Author: Aeronautical Research CouncilPublisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
Calculated lift distributions in incompressible flow on some sweptback wings
Author: J. A. BagleyCalculated Lift Slopes in Incompressible Flow for Certain Swept Wings
Author: G. M. JoyceThe Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
Author: Maxwell Alfred HeasletPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow
Author: M. J. QueijoPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 54
Book Description
A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived. The method requires that the span load at zero sideslip be known for the wing under consideration. Because this information is available for a variety of wings, this requirement should not seriously restrict the application of the present method. The basic method derived herein requires a mechanical differentiation and integration to obtain the rolling moment for the general wing in sideslip. For wings having straight leading and trailing edges over each semispan, the rolling moment equation in terms of plan-form parameters and the lateral center of pressure of the lift due to angle of attack. Calculated span loads and rolling-moment parameters are compared with experimental values. The comparison indicates good agreement between calculations and available experimental data.
The Calculation of Span Load Distributions on Swept-back Wings
Author: William MutterperlPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.
Theoretical and Experimental Pressure Distributions on Low Aspect Ratio Wings Oscillating in an Incompressible Flow
Author: William R. LaidlawPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 426
Book Description
High Speed Wing Theory
Author: Doris CohenPublisher: Princeton University Press
ISBN: 1400874947
Category : Technology & Engineering
Languages : en
Pages : 251
Book Description
Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author: A. van Heemert