Prediction of Airfoil Separated Flow Unsteady Aerodynamics

James A. Eley,; Sanford Fleeter,

doi:10.1515/TJJ.1991.8.3-4.185

Home Technology Prediction of Airfoil Separated Flow Unsteady Aerodynamics

Article

Licensed

Unlicensed Requires Authentication

Prediction of Airfoil Separated Flow Unsteady Aerodynamics

James A. Eley, and Sanford Fleeter,

Published/Copyright: December 1, 1991

Published by

Become an author with De Gruyter Brill

Author Information

From the journal International Journal of Turbo and Jet Engines Volume 8 Issue 3-4

MLA
APA
Harvard
Chicago
Vancouver

MLA
APA
Harvard
Chicago
Vancouver

Eley,, James A. and Fleeter,, Sanford. "Prediction of Airfoil Separated Flow Unsteady Aerodynamics" International Journal of Turbo and Jet Engines, vol. 8, no. 3-4, pp. 185-210. https://doi.org/10.1515/TJJ.1991.8.3-4.185

Eley,, J. & Fleeter,, S. (). Prediction of Airfoil Separated Flow Unsteady Aerodynamics. International Journal of Turbo and Jet Engines, 8(3-4), 185-210. https://doi.org/10.1515/TJJ.1991.8.3-4.185

Eley,, J. and Fleeter,, S. () Prediction of Airfoil Separated Flow Unsteady Aerodynamics. International Journal of Turbo and Jet Engines, Vol. 8 (Issue 3-4), pp. 185-210. https://doi.org/10.1515/TJJ.1991.8.3-4.185

Eley,, James A. and Fleeter,, Sanford. "Prediction of Airfoil Separated Flow Unsteady Aerodynamics" International Journal of Turbo and Jet Engines 8, no. 3-4 (): 185-210. https://doi.org/10.1515/TJJ.1991.8.3-4.185

Eley, J, Fleeter, S. Prediction of Airfoil Separated Flow Unsteady Aerodynamics. International Journal of Turbo and Jet Engines. ;8(3-4): 185-210. https://doi.org/10.1515/TJJ.1991.8.3-4.185

Copy

Copied to clipboard

BibTeX EndNote RIS

Published Online: 1991-12

You are currently not able to access this content.

Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula

Search journal Search the content of this journal

https://doi.org/10.1515/TJJ.1991.8.3-4.185

Articles in the same Issue

CONTENTS
Influence of Inlet Boundary Conditions on Turbulent Flowfield Computation
Prediction of Airfoil Separated Flow Unsteady Aerodynamics
Numerical Investigation of Thrust-Reversing Nozzles
Prediction of Heat Transfer Characteristics for Discrete Hole Film Cooling - One Row of Injection Into a Turbulent Boundary Layer
System Design Aspects of Propulsion Education in Aerospace Engineering Curricula