SYNOPTIC: Blunt Slender Cones in Viscous Hypersonic Flow

C.C. Horstman

doi:10.2514/3.49874

SYNOPTIC: Blunt Slender Cones in Viscous Hypersonic Flow

AIAA Journal ◽

10.2514/3.49874 ◽

1970 ◽

Vol 8 (10) ◽

pp. 1852-1852 ◽

Cited By ~ 1

Author(s):

C.C. Horstman

Keyword(s):

Hypersonic Flow ◽

Viscous Hypersonic Flow

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A Numerical Simulation of a 2D- Viscous Hypersonic Flow Using the Time-Marching Method of Characteristics

Notes on Numerical Fluid Mechanics (NNFM) - New Results in Numerical and Experimental Fluid Mechanics II ◽

10.1007/978-3-663-10901-3_48 ◽

1999 ◽

pp. 371-378

Author(s):

H. Sanaknaki ◽

J. Ballmann

Keyword(s):

Numerical Simulation ◽

Hypersonic Flow ◽

Method Of Characteristics ◽

Time Marching ◽

Viscous Hypersonic Flow ◽

Marching Method

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Stability derivatives of a oscillating wedges in viscous hypersonic flow

IOP Conference Series Materials Science and Engineering ◽

10.1088/1757-899x/370/1/012051 ◽

2018 ◽

Vol 370 ◽

pp. 012051

Author(s):

S Pavitra ◽

S Lavanya ◽

S A Khan

Keyword(s):

Hypersonic Flow ◽

Stability Derivatives ◽

Viscous Hypersonic Flow ◽

Derivatives Of

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An exploration of chemically reacting viscous hypersonic flow

Computer Methods in Applied Mechanics and Engineering ◽

10.1016/0045-7825(91)90039-9 ◽

1991 ◽

Vol 89 (1-3) ◽

pp. 85-128 ◽

Cited By ~ 10

Author(s):

John Argyris ◽

Ioannis St. Doltsinis ◽

Heinz Friz ◽

Jürgen Urban

Keyword(s):

Hypersonic Flow ◽

Viscous Hypersonic Flow ◽

Chemically Reacting

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Oscillating Slender Cone in Viscous Hypersonic Flow

AIAA Journal ◽

10.2514/3.50335 ◽

1972 ◽

Vol 10 (9) ◽

pp. 1139-1140 ◽

Cited By ~ 2

Author(s):

KAZIMIERZ J. ORLIK-RUCKEMANN

Keyword(s):

Hypersonic Flow ◽

Viscous Hypersonic Flow

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Stability Derivatives of Sharp Wedges in Viscous Hypersonic Flow

Aeronautical Quarterly ◽

10.1017/s0001925900005710 ◽

1971 ◽

Vol 22 (2) ◽

pp. 127-145 ◽

Cited By ~ 4

Author(s):

W. H. Hui ◽

R. A. East

Keyword(s):

Boundary Layer ◽

Perturbation Method ◽

Hypersonic Flow ◽

Bow Shock ◽

Vertex Angle ◽

Reflected Waves ◽

Displacement Boundary ◽

Stability Derivatives ◽

Viscous Hypersonic Flow ◽

Derivatives Of

SummaryUsing a perturbation method, the formulae for the pitching stability derivatives of sharp wedges at zero incidence in viscous hypersonic flow are obtained in closed form. The results include the effect of unsteady reflected waves from the bow shock and may be applied to any wedge provided that the bow shock is attached. The effect of viscosity of the gas is included in two parts: first, it thickens the wedge, thus introducing the concept of an effective wedge, thicker than the original wedge by a semi-vertex angle equal to the average inclination of the displacement boundary layer; secondly, it makes this effective wedge deformable. Comparison with previous theories is given.

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