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Hypersonic Research Vehicle (Hrv) Real-Time Flight Test Support Feasibility and Requirements Study. Part 1: Real-Time Flight Experiment Support
| AUTHOR | Nasa, National Aeronautics and Space Adm |
| PUBLISHER | Independently Published (10/18/2018) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The results are presented of a study to identify potential real time remote computational applications to support monitoring HRV flight test experiments along with definitions of preliminary requirements. A major expansion of the support capability available at Ames-Dryden was considered. The focus is on the use of extensive computation and data bases together with real time flight data to generate and present high level information to those monitoring the flight. Six examples were considered: (1) boundary layer transition location; (2) shock wave position estimation; (3) performance estimation; (4) surface temperature estimation; (5) critical structural stress estimation; and (6) stability estimation. Rediess, Herman A. and Ramnath, Rudrapatna V. and Vrable, Daniel L. and Hirvo, David H. and Mcmillen, Lowell D. and Osofsky, Irving B. Unspecified Center NAS2-12670; RTOP 505-66-00...
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Product Format
Product Details
ISBN-13:
9781728952468
ISBN-10:
1728952468
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
42
Carton Quantity:
97
Product Dimensions:
8.50 x 0.09 x 11.02 inches
Weight:
0.27 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Science | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
The results are presented of a study to identify potential real time remote computational applications to support monitoring HRV flight test experiments along with definitions of preliminary requirements. A major expansion of the support capability available at Ames-Dryden was considered. The focus is on the use of extensive computation and data bases together with real time flight data to generate and present high level information to those monitoring the flight. Six examples were considered: (1) boundary layer transition location; (2) shock wave position estimation; (3) performance estimation; (4) surface temperature estimation; (5) critical structural stress estimation; and (6) stability estimation. Rediess, Herman A. and Ramnath, Rudrapatna V. and Vrable, Daniel L. and Hirvo, David H. and Mcmillen, Lowell D. and Osofsky, Irving B. Unspecified Center NAS2-12670; RTOP 505-66-00...
Show More
