NASA NACA-RM-L7D11-1947 Wind-tunnel investigation of bomb-bay configurations intended to minimize the tumbling of light-weight bombs《旨在使轻质炸弹的歪斜最小化的炸弹湾结构的风洞研究》.pdf
《NASA NACA-RM-L7D11-1947 Wind-tunnel investigation of bomb-bay configurations intended to minimize the tumbling of light-weight bombs《旨在使轻质炸弹的歪斜最小化的炸弹湾结构的风洞研究》.pdf》由会员分享,可在线阅读,更多相关《NASA NACA-RM-L7D11-1947 Wind-tunnel investigation of bomb-bay configurations intended to minimize the tumbling of light-weight bombs《旨在使轻质炸弹的歪斜最小化的炸弹湾结构的风洞研究》.pdf(32页珍藏版)》请在麦多课文档分享上搜索。
1、RESEARCH MEMORANDUM - R,ichard E. Kuhn and Edward C. Polhamus L t Langley Memorial Aerormautical Laboratory Langley Field, Va. 3 NATIONAL 4 FOR ADVISORY COMMITTEE AERONAUTICS Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. I. . Provided by IHSNot f
2、or ResaleNo reproduction or networking permitted without license from IHS-,-,-The present investfgaticm coniated of a photographic study of the trajectories described by emall model bombs as they were released from a simulated bomb bay in a fuaelage modeL. The tests were con- ducted at two tmel apee
3、da and the effects of various deflectors, sep the- directIan and nature of the air flow within .the bombba is-.depicted as well as the bonib trajectorfes. The xqmbole .an reco- weye of the fhctuaticms of the static pressure at th points in the bmb bay (fig. 2) and %he results are preeeted in bBle I.
4、 .The Vnstallation. of cells in .the bamb bay (cdigktion coneiderably reduced the amputude of these f luctuatiom, especwly in the rear of the bonib by. ,. * Dm; measurements were also =de on some of the configurations and the drag Coefficients are presented in hble I. These drag coefficients Provide
5、d by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-are baaed 011 the wlw area of n.65 Square feet; the drag coefficient of the model with the bomb bay closod ie 0 .O35 tho drag coefficient .i of the wing alone ie 0.028 Attachfng deflectors. ahead of the bab ba
6、y materially increwed the drag. However, a wedgo-ahaped deflector gave the malleet increase in drag. t coNcLusIom- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-scrmbbas (fie. 3) A A A A A A A A A A A A A A A A A A A A A A A A F 10 -foot tunnel. r
7、I I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA RM No. L7DlI Fig. 2 I I NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS I I I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Fig. 3 NACA RM No. L7
8、Dll Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA RM No. L7Dll Fig. 4 I I fll “i 4.84 NATIONAL ADVlSORY COUMITTEE FOR AERONAUTICS Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Fig. 5 NACA RM
9、No. L7Dl1 NATIONAL ADVISORY COMHITTEE FOR AERONAUTICS . Y Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MACA RM No. L7Dl1 Fig. 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot fo
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