USAF Stability and Control Datcom PDF Download
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Languages : en
Pages :
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Author:
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Category :
Languages : en
Pages :
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Author: Douglas Aircraft Company
Publisher:
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Category : Stability of airplanes
Languages : en
Pages :
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Author: McDonnell Douglas Corporation. Douglas Aircraft Division
Publisher:
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Category : Airplanes
Languages : en
Pages :
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Author: John E. Williams
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 298
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Book Description
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in sections 4 through 7 of the USAF Stability and Control Datcom (revised January 1974). Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume I is the user's manual and presents program capabilities, input and output characteristics, and example problems. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author: Douglas Aircraft Company
Publisher:
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Category : Airplanes
Languages : en
Pages :
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Author: R. D. Finck
Publisher:
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Category : Airplanes
Languages : en
Pages :
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Author: Bandu N. Pamadi
Publisher: AIAA
ISBN: 9781600860997
Category : Aerodynamics
Languages : en
Pages : 810
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Author: Natalia M. Alexandrov
Publisher: SIAM
ISBN: 9780898713596
Category : Design
Languages : en
Pages : 476
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Book Description
Multidisciplinary design optimization (MDO) has recently emerged as a field of research and practice that brings together many previously disjointed disciplines and tools of engineering and mathematics. MDO can be described as a technology, environment, or methodology for the design of complex, coupled engineering systems, such as aircraft, automobiles, and other mechanisms, the behavior of which is determined by interacting subsystems.
Author:
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Category : Aeronautics
Languages : en
Pages : 244
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Author:
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Category :
Languages : en
Pages : 704
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