Accession Number : AD0055205


Title :   PART 2 - SWEPT WINGS - SUBSONIC FLUTTER MODEL TEST OF WINGS CARRYING HEAVY TIP PODS


Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY


Personal Author(s) : BRADY, W G ; MAIER, H G ; TARGOFF, WALTER P


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/055205.pdf


Report Date : Nov 1954


Pagination or Media Count : 103


Descriptors :   *SWEPT WINGS , *FLUTTER , LOAD DISTRIBUTION


Subject Categories : Aircraft
      Test Facilities, Equipment and Methods


Distribution Statement : APPROVED FOR PUBLIC RELEASE