Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /
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Author / Creator: | Hamilton, H. Harris, author. |
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Imprint: | Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September1980. |
Description: | 1 online resource (75 pages) : illustrations. |
Language: | English |
Series: | NASA technical paper ; 1698 NASA technical paper ; 1698. |
Subject: | Axisymmetric flow. Inviscid flow. Laminar heat transfer. Streamlined bodies. Three dimensional boundary layer. Boundary layer. Laminar flow. |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10914286 |
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100 | 1 | |a Hamilton, H. Harris, |e author. |0 http://id.loc.gov/authorities/names/n81025188 |1 http://viaf.org/viaf/45616656 | |
245 | 1 | 0 | |a Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue / |c H. Harris Hamilton II. |
260 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch, |c September1980. | ||
300 | |a 1 online resource (75 pages) : |b illustrations. | ||
336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
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490 | 1 | |a NASA technical paper ; |v 1698 | |
500 | |a Title from title screen (viewed on Aug. 10, 2016). | ||
500 | |a "September 1980." | ||
500 | |a "Performing Organization: NASA Langley Research Center"--Report documentation page. | ||
504 | |a Includes bibliographical references (pages 40-42). | ||
513 | |a Technical paper. | ||
536 | |a National Aeronautics and Space Administration |h 506-51-13-01 | ||
536 | |d L-13748 | ||
650 | 7 | |a Axisymmetric flow. |2 nasat | |
650 | 7 | |a Inviscid flow. |2 nasat | |
650 | 7 | |a Laminar heat transfer. |2 nasat | |
650 | 7 | |a Streamlined bodies. |2 nasat | |
650 | 7 | |a Three dimensional boundary layer. |2 nasat | |
650 | 7 | |a Boundary layer. |2 fast |0 (OCoLC)fst00837095 | |
650 | 7 | |a Laminar flow. |2 fast |0 (OCoLC)fst00991079 | |
710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://viaf.org/viaf/127305149 | |
710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Branch, |e issuing body. |0 http://id.loc.gov/authorities/names/n78091122 |1 http://viaf.org/viaf/269005387 | |
776 | 0 | 8 | |i Print version: |a Hamilton, H. Harris. |t Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue |w (OCoLC)7244662 |
776 | 0 | 8 | |i Microfiche version: |a Hamilton, H. Harris. |t Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue |w (OCoLC)711544592 |
830 | 0 | |a NASA technical paper ; |v 1698. | |
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