Accession Number : AD0009822


Title :   ON THE FLOW AT THE REAR OF A TWO-DIMENSIONAL SUPERSONIC AIRFOIL WITH THICKNESS


Corporate Author : PRINCETON UNIV NJ JAMES FORRESTAL RESEARCH CENTER


Personal Author(s) : PROBSTEIN, RONALD F


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/009822.pdf


Report Date : 01 May 1953


Pagination or Media Count : 6


Descriptors :   *SUPERSONIC AIRFOILS , MATHEMATICAL ANALYSIS , SUPERSONIC FLOW


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE