An Analysis of Acoustic Function and Navier-Stokes Equations in Aerodynamic
Acoustic function plays an important role in
aerodynamic mechanical engineering. It can classify the kind of
air-vehicle such as subsonic or supersonic. Acoustic velocity
relates with velocity and Mach number. Mach number relates
again acoustic stability or instability condition. Mach number
plays an important role in growth or decay in energy system.
Acoustic is a function of temperature and temperature is directly
proportional to pressure. If we control the pressure, we can control
acoustic function. To get pressure stability condition, we apply
Navier-Stokes equations.
[1] Chong Zhou and Joseph Majdalani, "Improved Mean-Flow Solution
for Slab Rocket Motor with Regressing Walls", (AIAA paper 2000-
3191).
[2] Jonathan C. French, "A Comparison of Nonlinear Combustion
Stability Mothods|".
[3] Flandro, G. A., and Majdalani, J., "Aeroacoustic Instability in
Rockets," AIAA Journal, Vol. 41, No. 3, 2003, pp. 485-497.
[4] Gary A. Flandro, "Aero-acoustic Instability in Rockets",AIAA
Journal Vol.41, No.3, March, 2003.
[5] Jonathan French, "Improvements to the Linear Standard Stability
Prediction Program (SSP)", (AIAA paper 2004-4181).
[6] Joseph M. Power, "Gas Dynamic," Aerodynamic II, Lecture Notes,
Department of Aerospace and Mechanical Engineering ,University of
North Dame 2003.
[7] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro, "Volume
to Surface Transformation of Rocket Stability Integrals", (AIAA
paper 2004-4053).
[8] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro, "Acoustic
Instability and Slab Rocket Motor", (AIAA paper 2004-4061).
[9] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro,
"Verification and Validation of Rocket Stability Integral
Transformation", (AIAA paper 2005-4001).
[10] S.M. Yahya, "Fundamental of Compressible Flow", May 2003, Third
Edition.
[11] Weidong Cai and V. Yang, "Turbulent Transport in Rocket Motor
Unsteady Flow field," Vol.185, Progress in Astronautics and
Aeronautic, 2000, pp-837-858.
[12] Yi Wang and Arnaud Trouve, "Artificial Acoustic Stiffness
Reduction in fully Compressible, Direct Numerical Simulation of
Combustion".
[1] Chong Zhou and Joseph Majdalani, "Improved Mean-Flow Solution
for Slab Rocket Motor with Regressing Walls", (AIAA paper 2000-
3191).
[2] Jonathan C. French, "A Comparison of Nonlinear Combustion
Stability Mothods|".
[3] Flandro, G. A., and Majdalani, J., "Aeroacoustic Instability in
Rockets," AIAA Journal, Vol. 41, No. 3, 2003, pp. 485-497.
[4] Gary A. Flandro, "Aero-acoustic Instability in Rockets",AIAA
Journal Vol.41, No.3, March, 2003.
[5] Jonathan French, "Improvements to the Linear Standard Stability
Prediction Program (SSP)", (AIAA paper 2004-4181).
[6] Joseph M. Power, "Gas Dynamic," Aerodynamic II, Lecture Notes,
Department of Aerospace and Mechanical Engineering ,University of
North Dame 2003.
[7] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro, "Volume
to Surface Transformation of Rocket Stability Integrals", (AIAA
paper 2004-4053).
[8] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro, "Acoustic
Instability and Slab Rocket Motor", (AIAA paper 2004-4061).
[9] Sean R. Fischbach, Joseph Majdalani, and Gary A. Flandro,
"Verification and Validation of Rocket Stability Integral
Transformation", (AIAA paper 2005-4001).
[10] S.M. Yahya, "Fundamental of Compressible Flow", May 2003, Third
Edition.
[11] Weidong Cai and V. Yang, "Turbulent Transport in Rocket Motor
Unsteady Flow field," Vol.185, Progress in Astronautics and
Aeronautic, 2000, pp-837-858.
[12] Yi Wang and Arnaud Trouve, "Artificial Acoustic Stiffness
Reduction in fully Compressible, Direct Numerical Simulation of
Combustion".
@article{"International Journal of Engineering, Mathematical and Physical Sciences:63325", author = "Hnin Hnin Kyi and Khaing Khaing Aye", title = "An Analysis of Acoustic Function and Navier-Stokes Equations in Aerodynamic", abstract = "Acoustic function plays an important role in
aerodynamic mechanical engineering. It can classify the kind of
air-vehicle such as subsonic or supersonic. Acoustic velocity
relates with velocity and Mach number. Mach number relates
again acoustic stability or instability condition. Mach number
plays an important role in growth or decay in energy system.
Acoustic is a function of temperature and temperature is directly
proportional to pressure. If we control the pressure, we can control
acoustic function. To get pressure stability condition, we apply
Navier-Stokes equations.", keywords = "Acoustic velocity, Irrotational, Mach number,Rotational.", volume = "2", number = "10", pages = "745-7", }