2857570

ESDU 73016 [ Active ]

The mean skin friction coefficient for a rough flat plate with a turbulent two-dimensional boundary layer in compressible adiabatic flow, with application to wedges, cylinders and cones.

standard by Engineering Sciences Data Unit , 07/01/1973

View all product details

Most Recent

Track It

Language:
    • Available Formats
    •  
    • Availability
    • Priced From ( in USD )
    • Secure PDF 🔒
    • Immediate download
    • $260.00
    • Add to Cart
    • Printed Edition
    • Ships in 1-2 business days
    • $325.00
    • Add to Cart

Customers Who Bought This Also Bought

 

About This Item

 

Full Description

ESDU 73016 gives curves and an equation for the value of Reynolds number based on distance along the plate above which an increase in roughness height will not affect skin friction drag. Also given are curves for the mean skin friction on an aerodynamically smooth, or a fully rough, plate at zero incidence for Mach numbers from 0 to 5 for various roughness heights. The use of the data for cylinders, and for cones and wedges in supersonic flow, is explained. Comparison with experimental data shows an r.m.s. error of 3 per cent in incompressible flow rising to 9 per cent for compressible adiabatic flow.

 

Product Details

Edition:
73
Published:
07/01/1973
Number of Pages:
17
File Size:
1 file , 350 KB
Product Code(s):
3, 3