Two-dimensional compression corner and planar shock wave interactions with a supersonic, turbulent boundary layer

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050 ⊔ 4 ‡aTL574.P7 ‡bL39 1975
086 0 ⊔ ‡aD 301.69/2:TR-75-0157
100 1 ⊔ ‡aLaw, C. Herbert, ‡eauthor.
245 1 0 ‡aTwo-dimensional compression corner and planar shock wave interactions with a supersonic, turbulent boundary layer / ‡cTheoretical Aerodynamics Research Laboratory (ARL) ; [author, C. Herbert Law].
264 ⊔ 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAerospace Research Laboratories, Air Force Systems Command, ‡c1975.
300 ⊔ ⊔ ‡aix, 107 pages : ‡billustrations ; ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
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490 0 ⊔ ‡aARL TR ‡v75-0157
500 ⊔ ⊔ ‡a"Final report, 1 August 1972-1 February 1975."
500 ⊔ ⊔ ‡a"June 1975."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (pages 70-71).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 7 ‡aTurbulent boundary layer. ‡2fast ‡0(OCoLC)fst01159225
650 ⊔ 7 ‡aShock waves. ‡2fast ‡0(OCoLC)fst01116729
650 ⊔ 7 ‡aAerodynamic load. ‡2fast ‡0(OCoLC)fst00798180
650 ⊔ 0 ‡aShock waves.
650 ⊔ 0 ‡aTurbulent boundary layer.
650 ⊔ 0 ‡aAerodynamic load.
710 2 ⊔ ‡aAerospace Research Laboratories (U.S.), ‡eissuing body.
710 2 ⊔ ‡aAerospace Research Laboratories (U.S.). ‡bTheoretical Aerodynamics Research Laboratory.
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