caa a22 4500 477044522 CHVBK 20180405111326.0 cr unu---uuuuu 170330e19960501xx s 000 0 eng 10.1007/BF01998465 doi (NATIONALLICENCE)springer-10.1007/BF01998465 The effect of heat and mass addition on the base pressure of bodies of revolution at supersonic speeds [Elektronische Daten] [A. Glagolev, A. Zubkov, A. Garanin, P. Tret'yakov] The results of an experimental investigation of the influence of mass addition and afterburning of combustion products of pyrotechnic mixtures in the base region of axisymmetric bodies in supersonic air flow at Mach numbers of 1.2-3.0 are reported. It is shown that the base-pressure increment increases monotonically to a maximum value with an optimum injected-mass flow rate. The value of this increment reduces as the Mach number decreases. A dependence generalizing the experimental data is presented. Plenum Publishing Corporation, 1996 Glagolev A. Institute of Mechanics, Moscow State University, 117234, Moscow aut Zubkov A. Institute of Mechanics, Moscow State University, 117234, Moscow aut Garanin A. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut Tret'yakov P. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut Combustion, Explosion and Shock Waves Kluwer Academic Publishers-Plenum Publishers 32/3(1996-05-01), 331-335 0010-5082 32:3<331 1996 32 10573 https://doi.org/10.1007/BF01998465 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01998465 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Glagolev A. Institute of Mechanics, Moscow State University, 117234, Moscow aut NATIONALLICENCE 700 1- Zubkov A. Institute of Mechanics, Moscow State University, 117234, Moscow aut NATIONALLICENCE 700 1- Garanin A. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut NATIONALLICENCE 700 1- Tret'yakov P. Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut NATIONALLICENCE 773 0- Combustion, Explosion and Shock Waves Kluwer Academic Publishers-Plenum Publishers 32/3(1996-05-01), 331-335 0010-5082 32:3<331 1996 32 10573 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer