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.

Corporate Author : MASSACHUSETTS INST OF TECH CAMBRIDGE AEROELASTIC AND STRUCTURES RESEARCH LAB

Personal Author(s) : LEE, ROBERT C.K. ; RUETENIK, J. RAY ; WITMER, EMMETT A.

Report Date : 01 AUG 1956

Pagination or Media Count : 1

Descriptors :   *AIRFOILS, *BLAST, *SHOCK WAVES, PROPAGATION, REFLECTION, SIMULATION.

Distribution Statement : APPROVED FOR PUBLIC RELEASE