Computational Simulation of Unsteady, Viscous, Hypersonic Flow about Flight Vehicles with Store Separation

2001 ◽  
Author(s):  
David L. Marcum
Keyword(s):  
Hypersonic Flow ◽  
Computational Simulation ◽  
Flight Vehicles ◽  
Store Separation ◽  
Viscous Hypersonic Flow

scholarly journals Development of lattice Boltzmann flux solver for simulation of hypersonic flow past flight vehicles

2018 ◽  
Vol 1053 ◽  
pp. 012073
Author(s):  
Zhuxuan Meng ◽  
Liming Yang ◽  
Chang Shu ◽  
Fan Hu ◽  
Donghui Wang ◽  
...  
Keyword(s):  
Hypersonic Flow ◽  
Lattice Boltzmann ◽  
Flight Vehicles ◽  
Flow Past

An exploration of chemically reacting viscous hypersonic flow

1991 ◽  
Vol 89 (1-3) ◽  
pp. 85-128 ◽  
Author(s):  
John Argyris ◽  
Ioannis St. Doltsinis ◽  
Heinz Friz ◽  
Jürgen Urban
Keyword(s):  
Hypersonic Flow ◽  
Viscous Hypersonic Flow ◽  
Chemically Reacting

Oscillating Slender Cone in Viscous Hypersonic Flow

AIAA Journal ◽  
1972 ◽  
Vol 10 (9) ◽  
pp. 1139-1140 ◽  
Author(s):  
KAZIMIERZ J. ORLIK-RUCKEMANN
Keyword(s):  
Hypersonic Flow ◽  
Viscous Hypersonic Flow

Stability Derivatives of Sharp Wedges in Viscous Hypersonic Flow

1971 ◽  
Vol 22 (2) ◽  
pp. 127-145 ◽  
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.

SYNOPTIC: Blunt Slender Cones in Viscous Hypersonic Flow

AIAA Journal ◽  
1970 ◽  
Vol 8 (10) ◽  
pp. 1852-1852 ◽  
Author(s):  
C.C. Horstman
Keyword(s):  
Hypersonic Flow ◽  
Viscous Hypersonic Flow
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