Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method

Download this report (PDF, 46.74 MB, 62 pages)
Report Number: WADC TR 54-383 Part 1
Author(s): Lee, Robert C. K., Witmer, Emmett A., Ruetenik, J . Ray
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Pages: 62
Contract: AF 33(038)-8906
DoD Project: 1350
DoD Task:
Identifier: AD0097323

Abstract:
The abstract for this report is either unavailable or has yet to be entered

Provenance: IIT

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement



Export