Accession Number:

AD0034208

Title:

THE WALL PRESSURE DISTRIBUTION IN A CHOKED TUNNEL

Descriptive Note:

Corporate Author:

AERONAUTICAL SYSTEMS DIV WRIGHT-PATTERSON AFB OH FLIGHT CONTROL LAB

Personal Author(s):

Report Date:

1953-12-01

Pagination or Media Count:

41.0

Abstract:

The wall pressure distribution in a choked tunnel is computed, following a method outlined previously. By the calculus of residues the solution is brought into such a form that its structure is displayed more clearly.

Subject Categories:

  • Photography
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE