Computational investigation of the compressible dynamic stall characteristics of the Sikorsky SSC-A09 airfoil
Authors
Johnston, Thomas A.
Subjects
Dynamic Stall
Supercritical Airfoil
Navier-Stokes Solution
Shock-induced Boundary Layer Separation
Supercritical Airfoil
Navier-Stokes Solution
Shock-induced Boundary Layer Separation
Advisors
Platzer, Max Franz
Ekaterinaris, J.A.
Date of Issue
1993-09
Date
September 1993
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Steady and unsteady two-dimensional flowfield analysis was conducted for a Sikorsky SSC-AO9 airfoil in compressible, high Reynolds number flows. Limited verification with experimental measurement was achieved. Computational methods included a steady, line
Type
Thesis
Description
Series/Report No
Department
Aeronautics and Astronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
252 p.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.