Accession Number : AD0092660


Title :   PRESSURE DISTRIBUTIONS AT MACH NUMBERS OF 1.6 AND 1.9 OF A CONICALLY CAMBERED WING OF TRIANGULAR PLAN FORM WITH AND WITHOUT PYLON-MOUNTED ENGINE NACELLES


Descriptive Note : Research memo.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC


Personal Author(s) : PHELPS, E R


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092660.pdf


Report Date : 20 Apr 1956


Pagination or Media Count : 39


Descriptors :   *DELTA WINGS , *ENGINE NACELLES , PRESSURE , DISTRIBUTION , SUPERSONIC FLOW


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE