Accession Number:

AD0097323

Title:

Shock-Tube Flow Investigation. Part 1. An Exploratory Study of the Generation of Blast-Type Profiles in the Shock Tube by the Reflection Method.

Descriptive Note:

Corporate Author:

MASSACHUSETTS INST OF TECH CAMBRIDGE AEROELASTIC AND STRUCTURES RESEARCH LAB

Report Date:

1956-08-01

Pagination or Media Count:

1.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE