Accession Number : AD0029123


Title :   Experimental Investigation of the Damping in Roll of Cruciform Triangular Wing-Body Combinations at Mach Numbers from 1.5 to 6.0


Descriptive Note : Research memo.


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


Personal Author(s) : Boissevain, Alfred G


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/029123.pdf


Report Date : 07 Apr 1954


Pagination or Media Count : 33


Descriptors :   *ROLL , *DELTA WINGS , BODIES OF REVOLUTION , CRUCIFORM WINGS , SUPERSONIC FLOW , HYPERSONIC CHARACTERISTICS


Subject Categories : Aircraft
      Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE