Aerodynamic characteristics of a body of revolution with gas-permeable surface areas

Journal of Applied Mechanics and Technical Physics

Volumn 51, Issue 1, 2010, Pages 65-73

  Fomin, V M ^a   Zapryagaev, V I ^a   Lokotko, A V ^a   Volkov, V F ^a   Lutskii, A E ^b   Men'shov, I S ^b   Maksimov, Yu M ^c   Kirdyashkin, A I ^c  

^a KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

^b KELDYSH INSTITUTE OF APPLIED MATHEMATICS   (Russian Federation)

^c Russian Academy of Medical Sciences   (Russian Federation)

Author keywords

Aerodynamic tests; Cone cylinder body of revolution; Drag coefficient; Gas permeable porous surface; Streamwise stability; Supersonic flow velocity

Indexed keywords

AERODYNAMIC CHARACTERISTICS; BODY OF REVOLUTION; EXPERIMENTAL STUDIES; NUMERICAL CALCULATION; PERMEABLE SURFACE; POROUS SURFACE; STATIC STABILITY;

AERODYNAMIC DRAG; CAPILLARY FLOW; CYLINDERS (SHAPES); DRAG COEFFICIENT; FLOW VELOCITY; GAS DYNAMICS; GASES; MACH NUMBER; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW;

AERODYNAMIC STABILITY;

EID: 76649134100     PISSN: 00218944     EISSN: 15738620     Source Type: Journal    
DOI: 10.1007/s10808-010-0010-5     Document Type: Article

References (13)

1. N. Frink, D. Bonhaus, V. Vatsa, et al., "A boundary condition for simulation of flow over porous surfaces," in: Proc. of the 19th Applied Aerodynamics Conf. (Anaheim, June 11-14, 2001), AIAA, Hampton (2001), pp. 2001-2412.
2. T. Hartman and J. M. Morgenstern, "Passive aerodynamic sonic boom suppression for supersonic aircraft," USA Patent No. 2004/0065774 A1 USA, Publ.04.08.04.
3. V. N. Zaikovskii, V. P. Kiselev, S. P. Kiselev, et al., "Effect of a porous insert in the supersonic part of the nozzle in changes in the nozzle thrust," Dokl. Ross. Akad. Nauk, 401, No. 4, 479-482 (2005).
4. N. I. Sidnyaev, "Review of methods for studying hypersonic gas flows past bodies with ablative coatings," Thermophys. Aeromech., 11, No. 4, 489-508 (2004).
5. A. I. Shvets and I. T. Shvets, Near-Wake Gas Dynamics [in Russian], Naukova Dumka, Kiev (1976).
6. J. E. Bowman and W. A. Clayden, "Cylindrical afterbodies in supersonic flow with gas ejection," AIAA J., 5, No. 8, 1524-1525 (1967).
7. D. M. Sykes, "Cylindrical and boat-tailed afterbodies in transonic flow with gas ejection," AIAA J., 8, No. 3, 588-590 (1970).
8. V. F. Zakharchenko and Yu. Kh. Kardanov, "Base pressure of bodies of revolution with gas ejection through the body surface into a supersonic flow," Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 163-167 (1983).
9. G. L. Grozdovskii, Yu. A. Lashkov, G. P. Svishchev, and I. N. Sokolova, "Effect of perforated inserts with streamwise slots on base pressure of a body of revolution at supersonic velocities," Uch. Zap. TsAGI, 3, No. 2, 21-26 (1972).
10. R. A. Yusupov, A. I. Kirdyashkin, and Yu. M. Maksimov, "Laws of SHS of porous composite ceramics and metal ceramics," Gorenie Plasmokhimiya, 1, No. 3, 351-356 (2004).
11. A. V. Lokotko, "Device for aerodynamic tests," Inventor's Certificate No. 1091703, MKI G 01 M 9/00, No. 3479000/40-23, Publ. 05. 10. 95, Bul. No. 13, Priority 08. 05. 82.
12. P. Chang, Separation of Flow, Pergamon Press, Oxford (1970).
13. N. F. Krasnov, Aerodynamics of Bodies of Revolution [in Russian], Mashinostroenie, Moscow (1964).