Skin friction measurements at a Mach number of three and momentum thickness Reynolds numbers up to a half million

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049 ‡aMAIN
050 4 ‡aTL574.F7 ‡bF5
086 0 ‡aD 301.45/46-2:79-3136
100 1 ‡aFiore, Anthony W., ‡eauthor.
245 1 0 ‡aSkin friction measurements at a Mach number of three and momentum thickness Reynolds numbers up to a half million / ‡cAnthony W. Fiore.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bFlight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, ‡c1980.
300 ‡axi, 60 pages : ‡billustrations ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAFFDL-TR ; ‡v79-3136
500 ‡aFinal report for period June 1976 to October 1979.
500 ‡aCover title.
500 ‡a"September 1980."
504 ‡aIncludes bibliographical references (pages 59-60).
538 ‡aMode of access: Internet.
650 7 ‡aTurbulent boundary layer. ‡2fast ‡0(OCoLC)fst01159225
650 7 ‡aSkin friction (Aerodynamics) ‡2fast ‡0(OCoLC)fst01120142
650 7 ‡aReynolds number. ‡2fast ‡0(OCoLC)fst01096833
650 0 ‡aReynolds number.
650 0 ‡aTurbulent boundary layer.
650 0 ‡aSkin friction (Aerodynamics)
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095313881
CID ‡a102856035
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