Tabulation of coordinates for hypersonic axisymmetric nozzles : Part 1, Analysis and coordinates for test section Mach numbers of 8, 12 and 20

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086 0 ‡aD 301.45/13:58-300/Part I
088 ‡aAD 204213
088 ‡aWADC TN 58-300, PART 1
100 1 ‡aCresci, Robert J., ‡eauthor.
245 1 0 ‡aTabulation of coordinates for hypersonic axisymmetric nozzles : ‡nPart 1, ‡pAnalysis and coordinates for test section Mach numbers of 8, 12 and 20 / ‡cRobert J. Cresci.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bWright Air Development Center, Air Research and Development Command, United States Air Force, ‡c1958.
300 ‡avii, 61 pages : ‡billustrations, figures, tables ; ‡c29 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aWADC TN ; ‡v58-300, PART 1
500 ‡a"Prepared for Wright Air Development Center, Aeronautical Research Laboratory, by Polytechnic Institute of Brooklyn, under Contract N. AF 33(616)-3978, Project No. 1363, Task No. 70129."
500 ‡a"ASTIA Document No. 204 213."
500 ‡a"October 1958."
504 ‡aIncludes bibliographical references (page 11).
538 ‡aMode of access: Internet.
583 1 ‡awill digitize ‡c20201022 ‡zQueued for digitization October 22, 2020 ‡5miu ‡2pda
650 0 ‡aAerodynamics, Hypersonic.
650 0 ‡aSupersonic nozzles.
710 1 ‡aUnited States. ‡bAir Force. ‡bAir Research and Development Command, ‡esponsor.
710 2 ‡aWright Air Development Center, ‡eissuing body.
710 2 ‡aPolytechnic Institute of Brooklyn. ‡bDepartment of Aeronautical Engineering and Applied Mechanics, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095330273 ‡cPart I (r: WADC-TN-300)
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