Accession Number : AD0029320


Title :   COMPARISON BETWEEN THEORY AND EXPERIMENT FOR INTERFERENCE PRESSURE FIELD BETWEEN WING AND BODY AT SUPERSONIC SPEEDS


Descriptive Note : Technical note


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER


Personal Author(s) : PITTS, WILLIAM C ; NIELSEN, JACK N ; GIONFRIDDO, MAURICE P


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/029320.pdf


Report Date : Apr 1954


Pagination or Media Count : 68


Descriptors :   *SUPERSONIC FLOW , *WINGS , INTERFERENCE , BODIES OF REVOLUTION , WING BODY CONFIGURATIONS , PRESSURE , DISTRIBUTION


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE