Download or read book A Pressure distribution Investigation of the Aerodynamic Characteristics of a Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers of 1 41 and 2 01 written by John P. Gapcynski and published by . This book was released on 1955 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The changes in the aerodynamic characteristics of a body of revolution with a fineness ratio of 8 have been determined at Mach numbers of 1.41 and 2.01, a Reynolds number, based on body length, of 4,540,000, and angles of incidence of 0 degrees and plus or minus 3 degrees as the position of the body is varied with respect to a reflection plane. The data are compared with theoretical results.

Download or read book Reports and Memoranda Aeronautical Research Council written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1967 with total page 938 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reports and Memoranda written by and published by . This book was released on 1967 with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

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 Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 1238 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Pressure distribution Investigation of a Fineness ratio 12 2 Parabolic Body of Revolution NACA RM 10 at M written by Morton Cooper and published by . This book was released on 1952 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Investigation of the Normal force Axial force and Pitching moment Characteristics of Blunt Low fineness ratio Bodies of Revolution at a Mach Number of 3 55 written by Russell W. McDearmon and published by . This book was released on 1961 with total page 36 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 Investigation of the Drag of Blunt nosed Bodies of Revolution in Free Flight at Mach Numbers from 0 6 to 2 3 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2 45 and 3 19 written by G. B. Marson and published by . This book was released on 1954 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Base Pressures Obtained from the X 15 Airplane at Mach Numbers from 1 1 to 3 2 written by Edwin J. Saltzman and published by . This book was released on 1961 with total page 32 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 Columbia Crew Survival Investigation Report written by Nasa and published by PDQ Press. This book was released on 2009 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA commissioned the Columbia Accident Investigation Board (CAIB) to conduct a thorough review of both the technical and the organizational causes of the loss of the Space Shuttle Columbia and her crew on February 1, 2003. The accident investigation that followed determined that a large piece of insulating foam from Columbia's external tank (ET) had come off during ascent and struck the leading edge of the left wing, causing critical damage. The damage was undetected during the mission. The Columbia accident was not survivable. After the Columbia Accident Investigation Board (CAIB) investigation regarding the cause of the accident was completed, further consideration produced the question of whether there were lessons to be learned about how to improve crew survival in the future. This investigation was performed with the belief that a comprehensive, respectful investigation could provide knowledge that can protect future crews in the worldwide community of human space flight. Additionally, in the course of the investigation, several areas of research were identified that could improve our understanding of both nominal space flight and future spacecraft accidents. This report is the first comprehensive, publicly available accident investigation report addressing crew survival for a human spacecraft mishap, and it provides key information for future crew survival investigations. The results of this investigation are intended to add meaning to the sacrifice of the crew's lives by making space flight safer for all future generations.

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 Government Reports Index written by and published by . This book was released on 1971 with total page 790 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Flow Past a Straight and a Swept wing body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1 0 written by W. F. Lindsey and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.