Download or read book Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1 57 to 2 86 written by Dennis E. Fuller and published by . This book was released on 1963 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1 57 to 2 86 written by Dennis E. Fuller and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers written by Linda S. Bangert and published by . This book was released on 1992 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of Afterbody Geometry on the Aerodynamic Characteristics of Rectangular Afterbodies at Transonic Mach Numbers written by Linda S. Bangert and published by . This book was released on 1991 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt: A parametric study was conducted in the Langley 16-Foot Transonic Tunnel on an isolated nonaxisymmetic fuselage model that simulates a twin-engine fighter. The effects of aft-end closure distribution (top/bottom) nozzle-flap boattail angle versus nozzle-sidewall boattail angle) and afterbody and nozzle corner treatment (sharp or radius) were investigated. Four different closure distributions with three different corner radii were tested. Tests were conducted over a range of Mach numbers from 0.40 to 1.25 and over a range of angles of attack from -3 to 9 degrees. Solid plume simulators were used to simulate the jet exhaust. For a given closure distribution in the range of Mach numbers tested, the sharp-corner nozzles generally had the highest drag, and the 2-in. corner-radius nozzles generally had the lowest drag. The effect of closure distribution on afterbody drag was highly dependent on configuration and flight condition. Bangert, Linda S. and Carson, George T., Jr. Langley Research Center NASA-TP-3236, L-17034, NAS 1.60:3236 RTOP 505-62-30-01...
Download or read book Calculated Pressure Distributions and Components of Total drag Coefficients for 18 Constant volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2 0 to 12 0 with Experimental Aerodynamic Characteristics for Three of the Bodies written by Louis S. Stiver and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0 6 to 3 0 and Angles of Attack from 0 to 180 Deg written by William B. Baker (Jr.) and published by . This book was released on 1976 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of Afterbody Geometry on the Aerodynamic Characteristics of Circular Bodies written by Asher Sigal and published by . This book was released on 1987 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1 6 to 4 6 written by and published by . This book was released on 1985 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness ratio 10 Cone Cylinder Configuration at Mach Numbers from 1 57 to 4 65 Including Design Parameter Curves for Circular Afterbody Flares written by A. B. Carraway and published by . This book was released on 1960 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of the B 1 Fuselage Afterbody Including Simulated Jet Exhaust Effects at Mach Numbers from 0 55 to 2 20 written by Earl A. Price (Jr.) and published by . This book was released on 1973 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics in Pitch of Several Ring wing body Configurations at a Mach Number of 2 2 written by Odell A. Morris and published by . This book was released on 1962 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics of Several High drag Bodies at Mach Numbers from 1 50 to 4 63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0 065 scale Model of a Four stage Rocket Configuration at Mach Numbers of 1 41 and 1 82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamics of Slender Bodies at Mach Number of 3 12 and Reynolds Numbers from 2 X 10 6 to 15 X 10 6 written by John R. Jack and published by . This book was released on 1954 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind tunnel Investigation of Effects of Noise Bluntness Face Shape and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2 37 2 98 and 3 90 written by and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
