Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-cylinder-flare Configuration in Free Flight at Mach Numbers Up to 4.7
Author | : Charles R. Rumsey |
Publisher | : |
Total Pages | : 66 |
Release | : 1961 |
Genre | : Fluid mechanics |
ISBN | : |
Download Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 47 full books in PDF, epub, and Kindle. Read online free Measurements Of Aerodynamic Heat Transfer On A 15 Degree Cone Cylinder Flare Configuration In Free Flight At Mach Numbers Up To 47 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Charles R. Rumsey |
Publisher | : |
Total Pages | : 66 |
Release | : 1961 |
Genre | : Fluid mechanics |
ISBN | : |
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 1766 |
Release | : 1961-07 |
Genre | : Technology |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 976 |
Release | : 1961 |
Genre | : Rocketry |
ISBN | : |
Beginning Oct. 1959 some issues include "Russian supplement."
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 448 |
Release | : 1960 |
Genre | : Aeronautics |
ISBN | : |
Author | : Great Britain. Stationery Office |
Publisher | : |
Total Pages | : 986 |
Release | : 1974 |
Genre | : Government publications |
ISBN | : |
Author | : Charles B. Rumsey |
Publisher | : |
Total Pages | : 26 |
Release | : 1955 |
Genre | : Aerodynamic heating |
ISBN | : |
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
Author | : Nasa |
Publisher | : PDQ Press |
Total Pages | : 400 |
Release | : 2009 |
Genre | : History |
ISBN | : 9780979828898 |
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.