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Yu.V. Shelud’ko (1980)
Measurement of base pressure of axisymmetric bodies of small aspect ratio
N.P. Mende (1980)
On a method of determining nonlinear aerodynamic forces and moments
Inverse problem of nonlinear ballistics. I. Planar motion N.P. Mende (1989)
N.P. Mende, Inverse problem of nonlinear ballistics. I. Planar motion, Prep. Ioffe PTI, No. 1326, Leningrad, 1989.
Estimation of the temperature and concentration of components in base region of the body with regard for non-equilibrium physical-chemical processes V.B. Knot’ko (1979)
V.B. Knot?ko, Estimation of the temperature and concentration of components in base region of the body with regard for non-equilibrium physical-chemical processes, Fluid Dyn., 1979, No. 1, P. 187?191.
Determination of turbulent base pressure in supersonic axisymmetric flow Muller (1969)
Questions of Rocket Technology
I.M. Dementiev (1979)
Shadow methods for visualization and registration of the motion of objects on ballistic setups
A.N. Lyubimov (1964)
Three-Dimensional Ideal Gas Flow Around Smooth Bodies
citation_title=of Supersonic Flow Visualization, citation_publication_date= (2000)
of Supersonic Flow Visualization
N.P. Mende S.V. Bobashev (2005)
Techniques of mathematical planning of ballistic experiment, IJ. Tech. Phys., 75
V.V. Nosov (1976)
On some peculiarities of aerodynamic characteristics of cones in viscous hypersonic flow
Spark Light Source I.M. Dementiev (1980)
I.M. Dementiev, Spark Light Source, Author Certificate No. 760240. Bulletin of Inventions No. 32, 1980.
A.N. Mikhalev P.I. Kovalev (1999)
Research of aerodynamic properties and flow field of hypervelocity elements on a ballistic traceJ. Tech. Phys., 69
P.G. Leutin V.G. Artonkin (1972)
V.G. Artonkin, P.G. Leutin, K.P. Petrov et al., Aerodynamic characteristics of sharp and blunted cones at subsonic and supersonic speeds, Trudy TsAGI, 1972, Iss. 1413.
R. Starr (1977)
Base pressure on sharp and blunt conical bodies at supersonic speedsAIAA Journal, 15
G.I. Mishin (1967)
Testing area for aerodynamic research
K.P. Petrov (1998)
Aerodynamics of the Bodies of Simplest Shapes
V. Knot'ko (1979)
Estimate of the temperature and concentrations of the components in the base region behind a body with allowance for nonequilibrium physicochemical processesFluid Dynamics, 14
Yu.V. Shelud’ko (1980)
Investigation of the Mach number influence on near-wake parameters of the cone
T.N. Canning Ballistic-Range Technology (1970)
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Tables of supersonic flow around cones Z. Kopal (1947)
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A.N. Mikhalev (1980)
On the influence of the Reynolds number on near-wake parameters of supersonic cones
Abstract Aerodynamic characteristics of a sharp cone with the semi-apex angle of 15° are investigated by the methods of ballistic modelling in the Mach number range from 0.5 to 3.7, which are computed under the assumption of their almost linear behavior at the angles of attack up to 10°. Using the direct shadow pictures the geometric characteristics of near wake are measured and analyzed within the considered transonic and supersonic range. They provide the basis for semi-empirical computation of integral parameters of the base cavity: the pressure, density, and temperature.
Thermophysics and Aeromechanics – Springer Journals
Published: Sep 1, 2008
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