1992-10-01

Analysis of the Effect of Heat Strips on Boundary Layer Development Over a Flat Plate 921923

Two dimensional fourth order boundary layer calculations were made for flows over a flat plate with and without flush mounted surface heating. Constant wall temperature, increasing wall temperature and decreasing wall temperature heating cases were studied for different surface heating lengths. The boundary layer properties; temperature, tangential velocity, normal velocity, vorticity and transition location were studied for these temperature distributions. The boundary layer results indicate that with the proper selection of surface temperature variation and length the transition location can be either increased or decreased. Modified boundary layer properties, due to heating are shown to persist well after heating is stopped, even when the flow is turbulent. The results indicate that this technique may be useful in modifying transition and separation locations over airfoils.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Theoretical Predication of Airfoil Drag Polars

680200

View Details

TECHNICAL PAPER

Studies of Friction Drag and Pressure Drag of Airfoils Using the Eppler Program

881396

View Details

JOURNAL ARTICLE

Improved RANS Computations of Flow over the 25°-Slant-Angle Ahmed Body

2017-01-1523

View Details

X