Abstract
Numerical simulation is used to study the gasdynamics of annular cumulative nozzles. The class of nozzles considered includes those with a flat-ended plug and plugs of different length. The thrust performance of cumulative nozzles is determined over wide ranges of the nozzle pressure ratio and the specific heat ratio and the ranges on which the self-adjustment effect takes place are established. It is found that for low nozzle pressure ratios the cumulative nozzle with a flat-ended plug provides greater thrust than a finite-length plug nozzle optimal for operation in a vacuum.
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REFERENCES
G. Hagemann, H. Immich, and M. Terhardt, "Flow phenomena in advanced rocket nozzles: the plug nozzle," AIAA Paper, No. 3522 (1998).
S.V. Baftalovskii, A. N. Kraiko, and N. I. Tillyayeva, "Designing self-adjustable plug nozzles optimal for operation in a vacuum," in: Proceedings of 22nd Scientific Symposium on Cosmonautics [in Russian], Voina i Mir, Moscow (1999), p. 116.
S.V. Baftalovskii, A. N. Kraiko, and N. I. Tillyayeva, "Optimal design of self-controlled spike nozzles and their thrust determination at start," AIAA Paper, No. 4955 (1999).
G. Dumnov, V. Klimov, and N. Ponomarev, "Investigation of linear plug layout of rocket engines for reusable launch vehicles," AIAA Paper, No. 3288 (2000).
M. E. N. Wisse and W. J. Bannink, "Half model restrictions for linear plug testing," AIAA J., 39, 2148 (2001).
J. J. Korte, A.O. Salas, H. J. Dunn, et al., "Multidisciplinary approach to linear Aerospike nozzle design," J. Propulsion Power, 17, 93 (2001).
A. N. Kraiko, N. I. Tillyayeva, and S.V. Baftalovskii, "Optimal design of plug nozzles and their thrust determination at start," J. Propulsion Power, 17, 1347 (2001).
V. I. Myshenkov and E.V. Myshenkov, "Numerical simulation of the outflow from a slotted centrifugal nozzle (Znamenskii nozzle)”, Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 5, 119 (1997).
E.V. Myshenkov and V. I. Myshenkov, "Numerical simulation of the outflow from a Znamenskii nozzle. Parametric study," Teplofiz. Vys. Temp., 37, 142 (1999).
T.N. Dombrovskaya, E.M. Kalinin, V. S. Maksimenkov, et al., "Experimental invesigation of the thrust performance of an annular slotted nozzle without a central body (centrifugal flow head)”, Kosmonavt. Raketostr., No. 17, 22 (1999).
P. R. Spallart and S. R. Allmaras, "A one-equation turbulencemodel for aerodynamic flows," Rech. A´erosp., No. 1, 5 (1994).
V. I. Kopchenov and A.N. Kraiko, "A monotonic second-order difference scheme for hyperbolic systems in two independent variables," Zh. Vychisl. Mat. Mat. Fiz., 23, 848 (1983).
E.V. Myshenkov and E.V. Myshenkova, "Technique of interactive grid adaptation for calculating viscous gasdynamic flows," Lesn. Vestn., No. 1 (21), 180 (2002).
A. N. Kraiko, E.V. Myshenkov, K. S. P'yankov, and N. I. Tillyayeva, "Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction," Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 5, 191 (2002).
A. N. Kraiko, A. S. Telyakovskii, and N. I. Tillyayeva, "Designing the optimal contour of a supersonic nozzle with appreciable flow deflection," Zh. Vychisl. Mat. Mat. Fiz., 34, 1444 (1994).
A. N. Kraiko, K. S. P'yankov, and N. I. Tillyayeva, "Profiling the supersonic part of a plug nozzle with a nonuniform transonic flow," Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 4, 145 (2002).
E.V. Myshenkov, E.V. Myshenkova, and N. I. Tillyayeva, "Calculation of cumulative nozzles with a short central body within the framework of the Reynolds equations," in: Abstracts of 4th Intern. Conf. on Nonequilibrium Processes in Nozzles and Jets (NPNJ-2002), St. Petersburg, 2002 [in Russian], Moscow Aviation Institute, Moscow (2002), p. 339.
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Myshenkov, E.V., Myshenkova, E.V. & Tillyayeva, N.I. Numerical Investigation of the Flows in Cumulative Short-Plug Nozzles within the Framework of the Reynolds Equations. Fluid Dynamics 38, 482–490 (2003). https://doi.org/10.1023/A:1025158425387
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DOI: https://doi.org/10.1023/A:1025158425387