Measurements of Flow Properties in the Vicinity of Three Wing-fuselage Combinations at Mach Numbers of 1.61 and 2.01
Author: Harry W. Carlson
Publisher:
Published: 1959
Total Pages: 78
ISBN-13:
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Author: Harry W. Carlson
Publisher:
Published: 1959
Total Pages: 78
ISBN-13:
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Publisher:
Published: 1959
Total Pages: 80
ISBN-13:
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Publisher:
Published: 1967
Total Pages: 1352
ISBN-13:
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Publisher:
Published: 1967
Total Pages: 986
ISBN-13:
DOWNLOAD EBOOKAuthor: Robert L. Weirich
Publisher:
Published: 1968
Total Pages: 148
ISBN-13:
DOWNLOAD EBOOKAuthor: Richard T. Whitcomb
Publisher:
Published: 1952
Total Pages: 60
ISBN-13:
DOWNLOAD EBOOKAuthor: Robert C. Nelson
Publisher: WCB/McGraw-Hill
Published: 1998
Total Pages: 441
ISBN-13: 9780071158381
DOWNLOAD EBOOKThe second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author: Nasa
Publisher: PDQ Press
Published: 2009
Total Pages: 400
ISBN-13: 9780979828898
DOWNLOAD EBOOKNASA 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.
Author: W. Z. Stepniewski
Publisher: Courier Corporation
Published: 2013-04-22
Total Pages: 640
ISBN-13: 0486318516
DOWNLOAD EBOOKDIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div