Accession Number : ADA197942


Title :   Dynamic Stall Computations Using a Zonal Navier-Stokes Model


Descriptive Note : Master's thesis


Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA


Personal Author(s) : Conroyd, Jr, Jack H


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a197942.pdf


Report Date : Jun 1988


Pagination or Media Count : 212


Abstract : A zonal Navier-Stokes model, is installed and verified on the NASA ames Cray X/MP-48 computer and is used to calculate the flow field about a NACA 0012 airfoil oscillating in pitch. Surface pressure distributions and integrated lift, pitching moment, and drag coefficient versus angle of attack are compared to existing experimental data for four cases and existing computational data for one case. These cases involve deep dynamic stall and fully detached flow at and below a freestream Mach number of .184. The flow field about the oscillating airfoil is investigated through the study of pressure, vorticity, local velocity and stream function. Finally, the effects of pitch rate on dynamic stall are investigated. Keywords: Theses, Computer programs, Dynamic stall, Navier Stokes, Unsteady aerodynamics.


Descriptors :   *AIRFOILS , *UNSTEADY FLOW , *STALLING , *NAVIER STOKES EQUATIONS , *AERODYNAMIC CHARACTERISTICS , PITCH(MOTION) , MODELS , DYNAMICS , RATES , THESES , MOMENTS , VORTICES , ANGLE OF ATTACK , FLOW FIELDS , SURFACE PROPERTIES , COEFFICIENTS , PRESSURE , MACH NUMBER , DRAG , LIFT , OSCILLATION , FREE STREAM , PRESSURE DISTRIBUTION , COMPUTATIONS , INTEGRATED SYSTEMS , EXPERIMENTAL DATA , FUNCTIONS(MATHEMATICS) , VELOCITY , COMPUTER PROGRAMS


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE