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Transonic Longitudinal Aerodynamic Characteristics Of Five Cone Cylinder Flare Bodies Of Revolution
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Book Synopsis Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution by :
Download or read book Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Static Aerodynamic Characteristics of a Blunt Cone-cylinder Body with Flared Afterbodies of Various Angles and Base Areas by : Roy M. Wakefield
Download or read book Transonic Static Aerodynamic Characteristics of a Blunt Cone-cylinder Body with Flared Afterbodies of Various Angles and Base Areas written by Roy M. Wakefield and published by . This book was released on 1959 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 by : George C. Ashby
Download or read book A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 written by George C. Ashby and published by . This book was released on 1965 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Square Flare on the Longitudinal Aerodynamic Characteristics of a Cone-cylinder at Mach Number 10 in Helium by :
Download or read book Effect of Square Flare on the Longitudinal Aerodynamic Characteristics of a Cone-cylinder at Mach Number 10 in Helium written by and published by . This book was released on 1968 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 by : Jim A. Penland
Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 written by Jim A. Penland and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle by :
Download or read book Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Static Aerodynamic Characteristics of Blunt Cone-cylinder Body with Flared Afterbodies of Various Angles and Base Areas [with List of References] by :
Download or read book Transonic Static Aerodynamic Characteristics of Blunt Cone-cylinder Body with Flared Afterbodies of Various Angles and Base Areas [with List of References] written by and published by . This book was released on 1959 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact by :
Download or read book Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact written by and published by . This book was released on 1961 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 by : Clyde Hayes
Download or read book Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics of 10 Short Axisymmetric Bodies at Mach Numbers of 5 to 15 by : Gary T. Chapman
Download or read book Experimental Aerodynamic Characteristics of 10 Short Axisymmetric Bodies at Mach Numbers of 5 to 15 written by Gary T. Chapman and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63 by : Dennis E. Fuller
Download or read book Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Asymmetric Lateral-directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack by : Paul L. Coe
Download or read book Asymmetric Lateral-directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack written by Paul L. Coe and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by : Leland Howard Jorgensen
Download or read book Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 written by Leland Howard Jorgensen and published by . This book was released on 1974 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of Aerodynamic Characteristics of Longitudinally Truncated Cylinders and Cone-Cylinders by : Rocco Girolamo
Download or read book An Experimental Study of Aerodynamic Characteristics of Longitudinally Truncated Cylinders and Cone-Cylinders written by Rocco Girolamo and published by . This book was released on 1975 with total page 73 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted at the Boston University supersonic wind-tunnel testing facility to determine the aerodynamic characteristics of the payload sections of sounding rockets designed to increase drag during re-entry. The higher drag is desired in order to increase the vehicle's atmospheric braking during re-entry so that its velocity is reduced to M=2 at a much higher altitude than is ordinarily attained. This would allow earlier parachute deployment, thus increasing airborne time and facilitating mid-air recovery by aircraft.
Book Synopsis An Investigation of the Static and Dynamic Aerodynamic Characteristics of a Series of Blunt-nosed Cylinder-flare Models at Mach Numbers from 0.65 to 2.20 by : David E. Jr Reese
Download or read book An Investigation of the Static and Dynamic Aerodynamic Characteristics of a Series of Blunt-nosed Cylinder-flare Models at Mach Numbers from 0.65 to 2.20 written by David E. Jr Reese and published by . This book was released on 1960 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Static Aerodynamic Characteristics of a Low Fineness Ratio Body of Revolution Having a Blunt Allipsoidal Nose and Flared Afterbodies of Various Angles and Base Areas by : Earl A. Knechtel
Download or read book Transonic Static Aerodynamic Characteristics of a Low Fineness Ratio Body of Revolution Having a Blunt Allipsoidal Nose and Flared Afterbodies of Various Angles and Base Areas written by Earl A. Knechtel and published by . This book was released on 1985 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 by : D. J. Spring
Download or read book The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 written by D. J. Spring and published by . This book was released on 1963 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes. (Author).