Preliminary study of effects of reynolds number and boundary-layer transition location on shock-induced separation /
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Corporate Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230],
National Aeronautics and Space Administration ;
1969
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Series: | NASA technical note ;
D-5003 |
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001 | dc17ee98-5865-436e-bddb-64532ee8cc19 | ||
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008 | 041012s1969 dcua b 000 0 eng d | ||
035 | |a (OCoLC-I)646277708 | ||
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035 | |a (Sirsi) o56716087 | ||
035 | |a (Sirsi) ocm56716087 | ||
040 | |a EGM |c EGM |d OCLCQ |d AD# | ||
086 | 0 | |a NAS 1.14:D-5003 | |
088 | |a NASA-TN-D-5003 | ||
100 | 1 | |a Blackwell, James A., |c Jr | |
245 | 1 | 0 | |a Preliminary study of effects of reynolds number and boundary-layer transition location on shock-induced separation / |c James A. Blackwell, Jr |
246 | 3 | |a NASA TN D-5003 | |
260 | |a Washington, D.C. : |b National Aeronautics and Space Administration ; |a [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], |c 1969 | ||
300 | |a 25 p. : |b ill. ; |c 27 cm | ||
490 | 1 | |a NASA technical note ; |v D-5003 | |
504 | |a Includes bibliographical references (p. 13) | ||
590 | |a Copy 1 bound with D-4984 |c 8602062 (parent record's ckey) |b 36105024751633 (item id) | ||
650 | 0 | |a Aerodynamics | |
650 | 0 | |a Reynolds number | |
650 | 0 | |a Viscous flow | |
650 | 0 | |a Wind tunnels | |
710 | 1 | |a United States |b National Aeronautics and Space Administration. | |
710 | 2 | |a Langley Research Center | |
830 | 0 | |a NASA technical note ; |v D-5003 | |
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