NASA NACA-TN-3466-1955 An investigation of the discharge and drag characteristics of auxiliary-air outlets discharging into a transonic stream《将辅助排气口放入跨音速流排放和阻力特性的研究》.pdf
《NASA NACA-TN-3466-1955 An investigation of the discharge and drag characteristics of auxiliary-air outlets discharging into a transonic stream《将辅助排气口放入跨音速流排放和阻力特性的研究》.pdf》由会员分享,可在线阅读,更多相关《NASA NACA-TN-3466-1955 An investigation of the discharge and drag characteristics of auxiliary-air outlets discharging into a transonic stream《将辅助排气口放入跨音速流排放和阻力特性的研究》.pdf(40页珍藏版)》请在麦多课文档分享上搜索。
1、.OVt “ “_!_.2_ M =TI-3. 00 .2 .4 .6 .8 1.0meVA1.0.8.6Ko.4:201I 4.o0 .2 .4 .6 .8 1.01.0.8.6K.4.20.M:.20 .2 4 .6 .8 1.0mpVAA/ i0 .2 .4 .6 .8 1.01.0.8.6.4.20/_j/ ;“i /M=I.50 .2 .4 .6 .8 t.0mevaFigure 9.- Discharge coefficient as a function of discharge flow ratiofor inclined outlets.Provided by IHSNot
2、for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACATN 9466 211.0.8.6KK.4.20i i0 .2 .4 .6 .8 1.0oCO- k/2i00 .2 .4IS. _/M = .0.6 .8 1.01.0 i.6 /.4 ,/ M=I,I.200 .2 .4 .6 .8 1.01.0.8.6K.4.20,S.2M_ .2I.C.8.6 Cf“.4 ,;_Y/Y.2 _ I00 .2M=I.3I0 .4 .6 .8 1.0 .4 .6 .8 1.0rn mioVA
3、oVAFigure ii.- Comparison of discharge coefficients of square and circularinclined outlets.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACATN 9466 29I.O, io0 .2 .4 .6 .8 1.0rTo I1% 4 ; Lrt, 5A- 41.0.8.6.4.20-1/ .!. .- 70 .2 .4 .6 .8 1.0ii/- - T-
4、!/M=I.21.0.8Figure i_.- Ratio of discharge coefficient to free-jet coefficient as afunction of discharge flow ratio for curved outlets.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_SNACA TN _466a.oI ITT.8 . _ i _ i00 .2 .4 ,6 .8 1.01.0.8,60.20 .2
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