Accession Number : AD0101819


Title :   AERODYNAMIC DERIVATIVES FOR TWO CROPPED DELTA WINGS AND ONE ARROWHEAD WING OSCILLATING IN DISTORTION MODES


Corporate Author : ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)


Personal Author(s) : WOODCOCK, D L


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/101819.pdf


Report Date : Apr 1956


Pagination or Media Count : 76


Descriptors :   *DELTA WINGS , UNITED KINGDOM , AERODYNAMIC CHARACTERISTICS , OSCILLATION


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE