Effect of Velocity Slip on the Burning Rate of Fuel Particles

[+] Author and Article Information
George Rudinger

Textron Bell Aerospace, Buffalo, N.Y.

J. Fluids Eng 97(3), 321-326 (Sep 01, 1975) (6 pages) doi:10.1115/1.3447310 History: Received June 05, 1975; Online October 12, 2010


The burning rate of fuel particles often is limited by the rate at which gaseous reactants can diffuse to the particle surface. Under such conditions, the diffusion limitation can be reduced by letting the particle slip with respect to the surrounding gas. The relationship between slip velocity and increase in the burning rate is analyzed taking into account both the decreasing particle size during combustion and the tendency of viscous drag to reduce slip. Four slip-producing flows are explored: shock waves, flow accelerations, flow oscillations (turbulence), and standing waves. Benefits are computed for a range of typical conditions. The results indicate that only small reductions in burning time can be expected for particle sizes suitable for flight applications.

Copyright © 1975 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In