Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air /
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| Author / Creator: | Scallion, William I., author. |
|---|---|
| Imprint: | Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1999. |
| Description: | 1 online resource (54 pages) : illustrations. |
| Language: | English |
| Series: | NASA TM- ; 1999-209357 NASA technical memorandum ; 1999-209357. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/11546968 |
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| 050 | 4 | |a TL521.3 |b .T3 no.1999- 209357 | |
| 074 | |a 0830-D (online) | ||
| 086 | 0 | |a NAS 1.15:209357 | |
| 100 | 1 | |a Scallion, William I., |e author. |0 http://id.loc.gov/authorities/names/no2006002073 |1 http://viaf.org/viaf/48973486 | |
| 245 | 1 | 0 | |a Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air / |c William I. Scallion. |
| 264 | 1 | |a Hampton, Virginia : |b National Aeronautics and Space Administration, Langley Research Center, |c September 1999. | |
| 300 | |a 1 online resource (54 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA TM- ; |v 1999-209357 | |
| 500 | |a "September 1999." | ||
| 500 | |a "Performing organization: NASA Langley Research Center"--Report documentation page. | ||
| 504 | |a Includes bibliographical references (page 9). | ||
| 513 | |a Technical memorandum. | ||
| 536 | |a Sponsored by the National Aeronautics and Space Administration |d WU 242-80-01-01 |d L-17867 | ||
| 588 | |a Description based on online resource; title from PDF title page (NASA, viewed Aug. 25, 2017). | ||
| 650 | 7 | |a Controllability. |2 nasat | |
| 650 | 7 | |a Effectiveness. |2 nasat | |
| 650 | 7 | |a Lifting bodies. |2 nasat | |
| 650 | 7 | |a Scale models. |2 nasat | |
| 650 | 7 | |a Wind tunnel tests. |2 nasat | |
| 650 | 7 | |a Elevons. |2 nasat | |
| 650 | 7 | |a Airplanes |x Flight testing. |2 fast |0 http://id.worldcat.org/fast/fst00803184 | |
| 650 | 7 | |a Lift (Aerodynamics) |2 fast |0 http://id.worldcat.org/fast/fst00998431 | |
| 710 | 2 | |a Langley Research Center, |e issuing body. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
| 776 | 0 | 8 | |i Print version: |a Scallion, William I. |t Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air |w (OCoLC)45191538 |
| 776 | 0 | 8 | |i Microfiche version: |a Scallion, William I. |t Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air |w (OCoLC)43642095 |
| 830 | 0 | |a NASA technical memorandum ; |v 1999-209357. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo84180 |y Government Printing Office |
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| 929 | |a eresource | ||
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| 928 | |t Library of Congress classification |a TL521.3 .T3 no.1999- 209357 |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/gpo84180 |z Government Printing Office |g ebooks |i 10890525 | ||