An airfoil flutter model suspension system to accomdate large static transonic airloads /
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| Author / Creator: | Reed, Wilmer H. |
|---|---|
| Imprint: | Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] |
| Description: | 1 online resource (36 p.) : ill. |
| Language: | English |
| Series: | NASA contractor report ; 177998 NASA-CR-177998 NASA contractor report ; NASA CR-177998. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/8770794 |
MARC
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| 086 | 0 | |a NAS 1.26:177998 | |
| 100 | 1 | |a Reed, Wilmer H. |0 http://id.loc.gov/authorities/names/n81026892 |1 http://viaf.org/viaf/67780519 | |
| 245 | 1 | 3 | |a An airfoil flutter model suspension system to accomdate large static transonic airloads / |c Wilmer H. Reed, III. |
| 260 | |a Newport News, VA : |b DEI-Tech, Inc. ; |a Hampton, Va. : |b National Aeronautics and Space Administration, Langley Research Center, |c [1985] | ||
| 300 | |a 1 online resource (36 p.) : |b ill. | ||
| 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 contractor report ; |v 177998 | |
| 490 | 1 | |a NASA-CR-177998 | |
| 500 | |a Title from title screen (viewed Apr. 10, 2012). | ||
| 500 | |a "October 1985." | ||
| 504 | |a Includes bibliographical references (p. 18-19). | ||
| 536 | |a Contract no. |b NAS1-17686 |d D-8402-3 |d 505-63-21-02 | ||
| 650 | 7 | |a Airfoils. |2 nasat | |
| 650 | 7 | |a Blowdown wind tunnels. |2 nasat | |
| 650 | 7 | |a Flutter analysis. |2 nasat | |
| 650 | 7 | |a Pressure distribution. |2 nasat | |
| 650 | 7 | |a Static pressure. |2 nasat | |
| 650 | 7 | |a Supercritical airfoils. |2 nasat | |
| 650 | 7 | |a Transonic wind tunnels. |2 nasat | |
| 650 | 7 | |a Two dimensional flow. |2 nasat | |
| 650 | 7 | |a Aerofoils. |2 fast |0 http://id.worldcat.org/fast/fst00798241 | |
| 650 | 7 | |a Transonic wind tunnels. |2 fast |0 http://id.worldcat.org/fast/fst01154888 | |
| 710 | 2 | |a DEI-Tech, Inc. |0 http://id.loc.gov/authorities/names/no2012050808 |1 http://viaf.org/viaf/249448500 | |
| 710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
| 776 | 0 | 8 | |i Print version: |a Reed, Wilmer H. |t airfoil flutter model suspension system to accomdate large static transonic airloads. |w (OCoLC)785222077 |
| 776 | 0 | 8 | |i Microfiche: |a Reed, Wilmer H. |t airfoil flutter model suspension system to accomdate large static transonic airloads. |w (OCoLC)466740867 |
| 830 | 0 | |a NASA contractor report ; |v NASA CR-177998. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo21276 |
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| 928 | |l Online |c UC-FullText |u http://purl.fdlp.gov/GPO/gpo21276 |g ebooks |i 7110776 | ||