Analytical contouring of pintle nozzle exit cone using computational fluid dynamics

Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations

Sanford Gordon, Bonnie McBride · NASA Technical Reports Server (NASA) · 1976 · 1.2K citations

Natural Sciences, Chemical Engineering, Physics +17

One- and Two-Phase Nozzle Flows

I-Shih Chang · AIAA Journal · 1980 · 84 citations

Engineering, Mechanical Engineering, Physics +16

A time-accurate implicit method for chemically reacting flows at allMach numbers

John Withington, Vigor Yang, Jian-Shun Shuen · 29th Aerospace Sciences Meeting · 1991 · 45 citations

Engineering, Chemical Engineering, Mechanical Engineering +17

Computation of two-phase viscous flow in solid rocket motors using aflux-split Eulerian-Lagrangian technique

M. Golafshani, HAI-TIEN LOH · 25th Joint Propulsion Conference · 1989 · 35 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Evaluation of preconditioning methods for time-marching systems

Jinzhang Feng, Charles Merkle · 28th Aerospace Sciences Meeting · 1990 · 31 citations

Computing, Computational Engineering, Mathematics +12