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 | : Robert Miserentino |
Publisher | : |
Total Pages | : 33 |
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 | : 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 | : 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 | : |
Publisher | : |
Total Pages | : 604 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1004 |
Release | : 1970 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : R. W. Rhudy |
Publisher | : |
Total Pages | : 106 |
Release | : 1971 |
Genre | : |
ISBN | : |
Download Drag and Performance Characteristics of Several Rigid Aerodynamic Decelerators at Mach Numbers from 1.5 to 6 Book in PDF, ePub and Kindle
Static-force tests were conducted at Mach numbers from 1.5 through 6 on rigid models of a supersonic X-2 parachute and two conical decelerators in the wake of cone-cylinder and ejection-seat forebodies. Surface pressure data were also obtained on the conical decelerators. The tests were made at decelerator angles of attack from -8 to 8 deg at free-stream dynamic pressures of 0.5, 1.0, 1.5, and 2.0 psia. The decelerators were positioned at various axial stations in the forebody wake, and selected configurations were tested in the free stream (no forebody). The data presented show how a rigid model of a flexible parachute can be used to obtain performance data in terms of static stability and drag coefficients. Agreement was obtained in axial-force coefficient for a rigid parachute model with a previously tested flexible model of the same configuration deployed behind the same forebody.
Author | : |
Publisher | : |
Total Pages | : 784 |
Release | : 1969-10 |
Genre | : Science |
ISBN | : |
Download U.S. Government Research & Development Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1416 |
Release | : 1970 |
Genre | : Science |
ISBN | : |
Download U. S. Government Research and Development Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1146 |
Release | : 1970 |
Genre | : Technology |
ISBN | : |
Download Government Reports Announcements Book in PDF, ePub and Kindle