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

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

Title: Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method
Date: 1956
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: WADC TR 54-383 Part 1
Creator: Lee, Robert C. K.; Witmer, Emmett A.; Ruetenik, J . Ray
Corporate Author: Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Extent: 62
Identifier: AD0097323
Access Rights: ASTIA
Distribution Classification: 1
Contract: AF 33(038)-8906
DoD Project: 1350
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFAL LTR
Report Availability: Full text available
Date Issued: 1956-08
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: IIT
Type: report
Format: 1 online resource