Accession Number : AD0142225

Title :   Transonic Flutter Model Tests. Part III. 60 Degree Delta Wings.

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s) : Calcerak, John C. ; Ostaszewski, Nicholas H.

Report Date : JAN 1958

Pagination or Media Count : 79

Descriptors :   *DELTA WINGS, *FLUTTER, TESTS, TRANSONIC CHARACTERISTICS.

Distribution Statement : APPROVED FOR PUBLIC RELEASE