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Effect of a conical break of delta-wings on the aerodynamic characteristics |
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| Authors: | A L Gonor V V Kravets A I Shvets |
| Institution: | (1) Moscow;(2) Dnepropetrovsk |
| Abstract: | The results of experimental investigations of the aerodynamic coefficients and the pressure on the windward face of delta-wings with a conical break are given. A comparison between the magnitudes of the aerodynamic quality of delta-wings with a conical break and models of a wing-cone with a  -shaped symmetrically grouped scheme is carried out at a Mach number of 5.96.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 100–104, November–December, 1976. |
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