Drag Characteristics Of Several Towed Decelerator Models At Mach 3 PDF Download
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Author | : Robert Miserentino |
Publisher | : |
Total Pages | : 46 |
Release | : 1970 |
Genre | : Acceleration (Mechanics) |
ISBN | : |
Download Drag Characteristics of Several Towed Decelerator Models at Mach 3 Book in PDF, ePub and Kindle
Drag characteristics of toroid-membrane and wide-angle conical shells used as towed decelerators.
Author | : James F. Campbell |
Publisher | : |
Total Pages | : 42 |
Release | : 1966 |
Genre | : Acceleration (Mechanics) |
ISBN | : |
Download Flow Field Survey and Decelerator Drag Characteristics in the Wake of a Model of the X-15 Airplane at Mach 2.30 and 4.65 Book in PDF, ePub and Kindle
Author | : John T. McShera |
Publisher | : |
Total Pages | : 32 |
Release | : 1963 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Aerodynamic Drag and Stability Characteristics of Towed Inflatable Decelerators at Supersonic Speeds Book in PDF, ePub and Kindle
Author | : Nickolai Charczenko |
Publisher | : |
Total Pages | : 30 |
Release | : 1962 |
Genre | : Aerodynamics |
ISBN | : |
Download Aerodynamic Characteristics of Towed Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65 Book in PDF, ePub and Kindle
Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).
Author | : |
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Total Pages | : 1004 |
Release | : 1970 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 604 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : E. G. Ewing |
Publisher | : |
Total Pages | : 502 |
Release | : 1979 |
Genre | : Parachutes |
ISBN | : |
Download Recovery System Design Guide Book in PDF, ePub and Kindle
This document serves as the third revision of the USAF Parachute Handbook which was first published in 1951. The data and information represent the current state of the art relative to recovery system design and development. The initial chapters describe representative recovery applications, components, subsystems, material, manufacture and testing. The final chapters provide empirical data and analytical methods useful for predicting performance and presenting a definitive design of selected components into a reliable recovery system.
Author | : |
Publisher | : |
Total Pages | : 300 |
Release | : 1972 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, ePub and Kindle
Author | : James F. Campbell |
Publisher | : |
Total Pages | : 44 |
Release | : 1967 |
Genre | : Aerodynamics |
ISBN | : |
Download Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 784 |
Release | : 1969-10 |
Genre | : Science |
ISBN | : |
Download U.S. Government Research & Development Reports Book in PDF, ePub and Kindle