Download or read book Aerox written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The AEROX program estimates lift, induced-drag and pitching moments to high angles (typ. 60 deg) for wings and for wingbody combinations with or without an aft horizontal tail. Minimum drag coefficients are not estimated, but may be input for inclusion in the total aerodynamic parameters which are output in listed and plotted formats. The theory, users' guide, test cases, and program listing are presented. Axelson, J. A. Ames Research Center NASA-TM-X-73208-VOL-1, A-6927-VOL-1 RTOP 505-06-19...

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Download or read book A Common Geometric Data base Approach for Computer aided Manufacturing of Wind tunnel Models and Theoretical Aerodynamic Analysis written by Michael J. See and published by . This book was released on 1983 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparisons of AEROX Computer Program Predictions of Lift and Induced Drag with Flight Test Data written by and published by . This book was released on 1981 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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Download or read book Automatic Control of Aircraft and Missiles written by John H. Blakelock and published by John Wiley & Sons. This book was released on 1991-09-03 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Second Edition continues the fine tradition of its predecessor by exploring the various automatic control systems in aircraft and on board missiles. Considerably expanded and updated, it now includes new or additional material on: the effectiveness of beta-beta feedback as a method of obtaining coordination during turns using the F-15 as the aircraft model; the root locus analysis of a generic acceleration autopilot used in many air-to-air and surface-to-air guided missiles; the guidance systems of the AIM-9L Sidewinder as well as bank-to-turn missiles; various types of guidance, including proportional navigation and line-of-sight and lead-angle command guidance; the coupling of the output of a director fire control system into the autopilot; the analysis of multivariable control systems; and methods for modeling the human pilot, plus the integration of the human pilot into an aircraft flight control system. Also features many new additions to the appendices.

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