33
Views
13
CrossRef citations to date
0
Altmetric
Original Articles

Flame Sheet Model for Stagnation Point Flows

&
Pages 377-388 | Received 28 Sep 1970, Published online: 10 May 2007

REFERENCES

  • Chung , P. M. , and Blankenship , V. D. , 1966 , Equilibrium Structure of Thin Diffusion Flame Zone , Phys. Fluids 9 , 1569 .
  • Bird , R. B. , Stewart , W. E. , and Lightfoot , E. N. , 1960 , Transport Phenomena , John Wiley and Sons, Inc. , New York .
  • Hayes , W. D. , and Probstein , R. F. , 1959 , Hypersonic Flow Theory , 288 – 291 , Academic Press , New York .
  • Hirschfelder , J. O. , Curtiss , C. F. , and Bird , R. B. , 1954 , Molecular Theory of Gases and Liquids , Wiley , New York .
  • Kassoy , D. R. , 1970 , On Boundary Layer Blow-Off , SIAMJ. ofApp. Math. 18 , 29 .
  • Libby , P. A. , and Pierucci , M. , 1964 , Laminar Boundary Layer with Hydrogen Injection Including Multicom-ponent Diffusion , AIAA J. 2 , 2118 .
  • Libby , P. A. , and Sepri , P. , 1967 , Laminar Boundary Layer with Complex Composition , Phys. Fluids 10 , 2138 .
  • Libby , P. A. , 1970 , On the Numerical Analysis of Stagnation Point Flows with Massive Blowing , AIAA J. 8 , 2095 .
  • Liu , T. M. , and Libby , P. A. , 1970 , Boundary Layer at a Stagnation Point with Hydrogen Injection , Comb. Sci. and Tech. 2 , 131 .
  • Penncr , S. S. , 1957 , Chemistry Problems in Jet Propulsion , 127 , Pergamon Press , New York .
  • Kadbill , J. R. , 1964 , Application of Quasilinearization to Boundary Layer Equations , AIAA J. 2 , 1860 .
  • Ruskol , V. A. , 1966 , Similar Solution of Laminar Boundary Equations with a Flame Front , Mek. Zhi. i Goza. 1 , 10 .
  • Sharma , O. P. , 1967 , Further Calculation for Hydrogen Injection into Laminar Boundary Layer Flow , Astro. Ada , 13 , 361 .
  • Svehla , R. A. , 1962 , Estimated Viscosities and Thermal Conductivities of Gases at High Temperature , NASA TR-1320 .
  • Tsuji , H. , and Yamaoka , J. , 1966 , Gasdynamic Analysis of Counter Flow Diffusion Flame in Forward Stagnation Region of Porous Cylinder , Tokyo Univ. , Institute of Space and Aeronautical Science Rep. No. 707 , pp. 95 – 115 .

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.