Accession Number : AD0092661


Title :   EFFECT OF MACH NUMBER ON BOUNDARY-LAYER TRANSITION IN THE PRESENCE OF PRESSURE RISE AND SURFACE ROUGHNESS ON AN OGIVE-CYLINDER BODY WITH COLD WALL CONDITIONS


Descriptive Note : Research memorandum


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC


Personal Author(s) : CARROS, ROBERT J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092661.pdf


Report Date : 20 Apr 1956


Pagination or Media Count : 34


Descriptors :   *BODIES OF REVOLUTION , *BOUNDARY LAYER , OGIVES , HYPERSONIC FLOW , MACH NUMBER , CYLINDRICAL BODIES , SUPERSONIC FLOW


Subject Categories : Theoretical Mathematics
      Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE