Accession Number : AD0101927

Title :   A METHOD FOR CALCULATING TURBULENT BOUNDARY LAYER DEVELOPMENT IN SUPERSONIC AND HYPERSONIC NOZZLES INCLUDING THE EFFECTS OF HEAT TRANSFER

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : PERSH, JEROME ; LEE, ROLAND

Report Date : 07 JUN 1956

Pagination or Media Count : 41

Descriptors :   *TURBULENT BOUNDARY LAYER, HYPERSONIC NOZZLES, MATHEMATICAL ANALYSIS, SUPERSONIC NOZZLES.

Distribution Statement : APPROVED FOR PUBLIC RELEASE