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- W2006174580 abstract "A model test program was conducted at 0.8 Macii number to examine important parameters in aircraft aft fuselage design. Thirteen twin jet interfairings were used to determine effects of interfairing length, interfairing base area, and engine spacing (combined with changes in maximum area and forebody shape). Three single jet configurations provided the effects of boattailing and served as a baseline for the twin jet tests. All configurations used a convergent (iris type) nozzle operating at a pressure ratio of 3.0. Test results show an optimum subsonic twin jet interfairing to be one that ends near the nozzle exit with zero base area. Small amounts of base area (3-8% of the maximum area) completely offset the favorable effects of interference between the exhaust jet and the freestream. Although geometrical changes that go along with increased engine spacing (larger maximum area, wider interfairing and flared forebody) tend to increase total drag, the effects on interference were small. Favorable interference levels, better than those of an equivalent pod, were obtained for all twin jet spacing ratios tested (S/DENG = 1.17, 1.43, and 2.37). It appears that the effects of increased spacing alone might be beneficial to afterbody performance." @default.
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- W2006174580 date "1970-05-01" @default.
- W2006174580 modified "2023-09-23" @default.
- W2006174580 title "Subsonic interference characteristics of single and twin jet afterbodies" @default.
- W2006174580 doi "https://doi.org/10.2514/3.44157" @default.
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