Download or read book A Wind tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2 37 2 98 and 3 90 at Angles of Attack to 90 Deg written by and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind Tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2 37 2 98 and 3 90 written by Fred M. Smith and published by . This book was released on 1960 with total page 35 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:
Download or read book Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0 25 to 2 written by and published by . This book was released on 1975 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of Two Bodies of Revolution with Noses of Varying Spherical Bluntness at Mach Numbers from 0 6 to 1 5 written by E. G Allee (Jr) and published by . This book was released on 1973 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel investigation was conducted to determine the static stability characteristics of two bodies of revolution fitted with 2-, 3-, and 4-cal tangent ogive noses of varying spherical bluntness. Testing was conducted at Mach numbers from 0.6 to 1.5 and angles of attack from -2 to 14 deg. The major effect of blunting the noses was evidenced in the axial-force coefficient. Lengthening the noses from 2 to 4 cal caused a forward movement of the center-of-pressure location and a corresponding decrease in axial-force coefficient at Mach numbers of 1.0 and higher. Changing from a 5- to a 9-cal midbody resulted in an increase in axial-force coefficient and an aft movement of the center-of-pressure location. (Author).
Download or read book A Wind Tunnel Investigation of Effects of Nose Bluntness Face Shape and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2 37 2 93 and 3 90 written by Fred L. Smith and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 0 20 to 1 17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule written by and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 written by and published by . This book was released on 1979 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 3 0 to 6 8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations written by and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive cylinder Model at Mach Numbers 1 75 to 4 50 written by Neil Arthur Zarin and published by . This book was released on 1964 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Assymtric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 degrees and Mach Numbers to 2 written by Robert L. Kruse and published by . This book was released on 1979 with total page 93 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Introduction to Vortex Dynamics written by and published by . This book was released on 1986 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Wind tunnel Force and Flow Visualization Data at Mach Numbers from 1 6 to 4 63 for a Series of Bodies of Revolution at Angles of Attack from 4 to 60 written by Emma Jean Landrum and published by . This book was released on 1979 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Pressure Data at Mach Numbers from 1 6 to 4 63 for a Series of Bodies of Revolution at Angles of Attack from 4 to 60 written by Emma Jean Landrum and published by . This book was released on 1977 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at a Mach Number of 2 91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90 written by John E. Grimaud and published by . This book was released on 1961 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:
