TY - GEN
T1 - The effect of first- and second-order slip condition on oscillatory flows
T2 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
AU - Zhang, Zheming
AU - Agarwal, Ramesh K.
PY - 2014
Y1 - 2014
N2 - In last two decades, several studies have been conducted to understand the molecular mechanism of slip of fluids (both liquids and gases) at a solid wall. Most of these studies have dealt with steady flow. Recently, Thalakkottor and Mohseni have shown by molecular dynamics simulations that in unsteady flow there is an additional slip above the slip observed in the steady flow. They have developed an unsteady slip flow model by extending the Maxwell's slip theory for steady flows to encapsulate unsteady flows. The model indicates that the slip velocity of a fluid in unsteady flow is also a function of the acceleration of the fluid in addition to its shear rate. Thus the slip velocity is both a function of first- and second-order derivatives normal to the wall multiplied by different coefficients dependent upon the nature of the fluid (liquid or gas). In this paper, we consider several unsteady flows - the Stokes flow, the Couette flow, and flow in a channel due to an oscillatory wall. In addition, we consider unsteady flow due to an impulsively started flat plate. Exact solutions are obtained by using the most general form of slip boundary condition that contains both first and second-order derivatives normal to the boundary. The coefficients that multiply these derivatives can be determined by knowledge of the nature of the fluid. It should be noted that these solutions can also be reduced to steady flows with slip with higher-order slip boundary condition that includes both first- and second-order derivatives normal to the wall.
AB - In last two decades, several studies have been conducted to understand the molecular mechanism of slip of fluids (both liquids and gases) at a solid wall. Most of these studies have dealt with steady flow. Recently, Thalakkottor and Mohseni have shown by molecular dynamics simulations that in unsteady flow there is an additional slip above the slip observed in the steady flow. They have developed an unsteady slip flow model by extending the Maxwell's slip theory for steady flows to encapsulate unsteady flows. The model indicates that the slip velocity of a fluid in unsteady flow is also a function of the acceleration of the fluid in addition to its shear rate. Thus the slip velocity is both a function of first- and second-order derivatives normal to the wall multiplied by different coefficients dependent upon the nature of the fluid (liquid or gas). In this paper, we consider several unsteady flows - the Stokes flow, the Couette flow, and flow in a channel due to an oscillatory wall. In addition, we consider unsteady flow due to an impulsively started flat plate. Exact solutions are obtained by using the most general form of slip boundary condition that contains both first and second-order derivatives normal to the boundary. The coefficients that multiply these derivatives can be determined by knowledge of the nature of the fluid. It should be noted that these solutions can also be reduced to steady flows with slip with higher-order slip boundary condition that includes both first- and second-order derivatives normal to the wall.
UR - http://www.scopus.com/inward/record.url?scp=85088344531&partnerID=8YFLogxK
U2 - 10.2514/6.2014-1443
DO - 10.2514/6.2014-1443
M3 - Conference contribution
AN - SCOPUS:85088344531
SN - 9781624102561
T3 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
BT - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
PB - American Institute of Aeronautics and Astronautics Inc.
Y2 - 13 January 2014 through 17 January 2014
ER -