Space Shuttle Hypersonic Aerodynamic And Aerothermodynamic Flight Research And The Comparison To Ground Test Results PDF Download
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Author | : Kenneth W. Iliff |
Publisher | : |
Total Pages | : 34 |
Release | : 1993 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Space Shuttle Hypersonic Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1064 |
Release | : 2010 |
Genre | : Aeronautics |
ISBN | : |
Download NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research Book in PDF, ePub and Kindle
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Author | : |
Publisher | : |
Total Pages | : 836 |
Release | : 1994 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
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Publisher | : |
Total Pages | : 1066 |
Release | : 2011 |
Genre | : |
ISBN | : |
Download NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1064 |
Release | : 1994 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalogue, United States Public Documents Book in PDF, ePub and Kindle
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Total Pages | : |
Release | : 1994 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 46 |
Release | : 1995 |
Genre | : |
ISBN | : |
Download A Comparison of Hypersonic Vehicle Flight and Prediction Results Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 392 |
Release | : 1994 |
Genre | : |
ISBN | : |
Download Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) Book in PDF, ePub and Kindle
Author | : Kenneth W. Iliff |
Publisher | : History Office |
Total Pages | : 432 |
Release | : 2004 |
Genre | : Biography & Autobiography |
ISBN | : |
Download From Runway to Orbit Book in PDF, ePub and Kindle
NOTE: NO FURTHER DISCOUNT FOR THIS PRINT PRODUCT--OVERSTOCK SALE -- Significantly reduced list price while supplies last NASA SP 2004-4109. NASA History Series. Presents the memoirs of Dr. Kenneth W. Iliff, the retired Chief Scientist of NASA Dryden Flight Research Center. He worked at NASA from 1962-2002. Related products: Commercial Orbital Transportation Services: A New Era in Spaceflight is available here: https: //bookstore.gpo.gov/products/sku/033-000-01367-1 Reference Guide to the International Space Station is available here: https: //bookstore.gpo.gov/products/sku/033-000-01373-6 Other products produced by the U.S. National Aeronautics and Space Administration (NASA) can be found here: https: //bookstore.gpo.gov/agency/550"
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Total Pages | : 37 |
Release | : 1994 |
Genre | : |
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Download Hypersonic Flight Testing Book in PDF, ePub and Kindle
The challenges of hypersonic system development require a combination of integrated ground testing, flight testing, and computational/simulation approaches. This report addresses the role of flight testing in the triad of development approach and is sub-divided into three parts: Propulsion, Aerothermal and Extrapolation of ground test data to flight. The reasons for propulsion flight test are illustrated by specific mini-case studies. The second part reviews some of the fundamental issues of flight testing and provides an overview of the aerothermal techniques. Specific examples include heat-transfer gage measurements and some of the common problems that have been encountered. The third part of this report discusses the initial flights of the Space Shuttle which uncovered a number of differences between preflight aerodynamic predictions and actual flight data. Most notable among these discrepancies was for longitudinal trim during high-speed re-entry. To investigate these differences, several computer codes were applied to a modified Space Shuttle Orbiter to determine aerodynamic parameters over a wide range of conditions. Computations were carried out for wind tunnel conditions and flight conditions to assess Mach number, real gas, and viscous effects on the reentry aerodynamics of the orbiter. flight-testing, Aerothermal techniques, Hypersonic vehicles, Computational Fluid Dynamics (CFD) simulations, High-speed re-entry.