Accession Number : AD0079113

Title :   ON THE HEAT TRANSFER TO THE WALLS OF A SHOCK TUBE

Corporate Author : CORNELL UNIV ITHACA NY GRADUATE SCHOOL OF AEROSPACE ENGINEERING

Personal Author(s) : ROTT, N. ; HARTUNIAN, R.

Report Date : NOV 1955

Pagination or Media Count : 47

Descriptors :   *LAMINAR BOUNDARY LAYER, *SHOCK TUBES, HEAT TRANSFER.

Distribution Statement : APPROVED FOR PUBLIC RELEASE