Injection of particles through a jet nozzle laterally into a supersonic airstream

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049 ‡aMAIN
086 0 ‡aD 301.45/33-2:64-181
100 1 ‡aHilliard, E. E., ‡eauthor.
245 1 0 ‡aInjection of particles through a jet nozzle laterally into a supersonic airstream / ‡cby E.E. Hilliard.
264 1 ‡aArnold Air Force Station, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1964.
300 ‡a12 pages : ‡billustrations, ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAEDC-TDR ; ‡v64-181
500 ‡a"September 1964."
504 ‡aIncludes bibliograqphic references (page 1).
520 ‡aTests were conducted in the 12-in. supersonic tunnel of the von Karman Gas Dynamics Facility to determine the particle distributions downstream of a nozzle exhausting particle-laden flow laterally into the airstream from the tunnel floor. Data were obtained at Mach 3 for a range of jet pressure ratios and nozzle sizes with the nozzles located at several positions upstream of the sampling rake. Reynolds number ranged from 0.15 to 0.62 X 10 to the sixth power per inch. Selected results are presented. (Author).
536 ‡aReport prepared by ARO, Inc., under Air Force Contract No. ‡bAF 40(600)-1000.
538 ‡aMode of access: Internet.
650 0 ‡aJets ‡xFluid dynamics.
650 0 ‡aSupersonic nozzles.
710 2 ‡aARO, Inc., ‡esponsor.
710 2 ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015104951747
CID ‡a102893358
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DAT 2 ‡a2024-07-29T17:30:02Z
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