MODELING OF CHAMBER FLOW FIELD OF SOLID ROCKET MOTORS WITH EROSIVE BURNING

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MANESHIAN M.A.; AKBARI M.H.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Seminar Paper

Paper Information

Seminar: FUEL AND COMBUSTION CONFERENCE OF IRAN
Year:2008 | Issue:2

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Title

MODELING OF CHAMBER FLOW FIELD OF SOLID ROCKET MOTORS WITH EROSIVE BURNING

Author(s)

MANESHIAN M.A. | AKBARI M.H.

Keywords

SOLID ROCKET MOTOR

EROSIVE BURNING

EULER EQUATIONS

MACCORMACK SCHEME

Abstract

THE PERFORMANCE OF A SOLID ROCKET MOTOR DEPENDS HEAVILY ON THE FLOW CHARACTERISTICS, THE CHEMICAL COMPOSITION OF THE GRAIN, COMBUSTION PRODUCTS AND THE BURNING RATE. IN THIS STUDY THE START-UP TRANSIENT INTERNAL BALLISTICS OF A TYPICAL SOLID ROCKET MOTOR (SRM) IS NUMERICALLY SIMULATED. TWO BURNING RATE LAWS ARE USED TO MODEL SIMPLE AND EROSIVE BURNING. GOVERNING EQUATIONS OF 2 -DIMENSIONAL IN VISCID FLOW ARE SOLVED USING AN EXPLICIT MACCORMACK FINITE DIFFERENCE TECHNIQUE IN WHICH THE LOCATIONS OF SHOCK WAVES ARE CAPTURED BY THE SOLUTION SCHEME. EROSIVE BURNING INCREASES THE CHAMBER PRESSURE AND THRUST DURING THE EARLY PORTION OF BURNING FOR A PARTICULAR MOTOR.

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APA: Copy

MANESHIAN, M.A., & AKBARI, M.H.. (2008). MODELING OF CHAMBER FLOW FIELD OF SOLID ROCKET MOTORS WITH EROSIVE BURNING. FUEL AND COMBUSTION CONFERENCE OF IRAN. SID. https://sid.ir/paper/906349/en

Vancouver: Copy

MANESHIAN M.A., AKBARI M.H.. MODELING OF CHAMBER FLOW FIELD OF SOLID ROCKET MOTORS WITH EROSIVE BURNING. 2008. Available from: https://sid.ir/paper/906349/en

IEEE: Copy

M.A. MANESHIAN, and M.H. AKBARI, “MODELING OF CHAMBER FLOW FIELD OF SOLID ROCKET MOTORS WITH EROSIVE BURNING,” presented at the FUEL AND COMBUSTION CONFERENCE OF IRAN. 2008, [Online]. Available: https://sid.ir/paper/906349/en

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