Accession Number:

AD0405843

Title:

SHOCK TUBE TEST TIME LIMITATION DUE TO TURBULENT WALL BOUNDARY LAYER

Descriptive Note:

Corporate Author:

AEROSPACE CORP EL SEGUNDO CA

Personal Author(s):

Report Date:

1963-05-06

Pagination or Media Count:

63.0

Abstract:

Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent wall boundary layers. The results are compared with those for wholly laminar wall boundary layers. Working curves are presented for more accurate estimates of test time in specific cases.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE