Performance analysis of secondary gas injection into a conical rocket nozzle

Journal of Propulsion and Power

Volumn 18, Issue 3, 2002, Pages 585-591

  Ko, Hyun ^a   Yoon, Woong Sup ^a  

^a Yonsei University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; JETS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; NOZZLES; SHOCK WAVES; TRAJECTORIES; TURBULENCE;

GAS INJECTION; THRUST VECTOR CONTROL (TVC);

ROCKETS;

EID: 0036575131     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5972     Document Type: Article

References (18)

1. Analysis of fluid mechanics of secondary injection for thrust vector control
2. Influence of injectant properties for fluid injection thrust vector control
3. Approximate analysis of thrust vector control by fluid injection
4. Comparison of Euler and Navier-Stokes solutions for nozzle flows with secondary injection
5. On secondary gas injection in supersonic flow
6. Analysis of performance of a hot gas injection thrust vector control system
7. Computational analysis of an axisymmetric fluidic injection nozzle
8. Predictions of channel and boundary-layer flows with a low-Reynolds-number turbulence model
9. The analysis and modeling of dilatational terms in compressible turbulence
10. Dilatation dissipation: The concept and application in modeling compressible mixing layers
11. Thin layer approximation and algebraic model for separated flow
12. Implicit factored scheme for the compressible Navier-Stokes equations
13. Secondary gas injection into a supersonic conical nozzle
14. Experiments on rocket thrust vector control by hot gas injection
15. Interaction of secondary injectants and rocket exhausts for thrust vector control