Accession Number : AD0218737

Title :   TESTING TECHNIQUE USED FOR FLUTTER TESTS OF MIT SEMI-SPAN WING MODELS AT SUPERSONIC SPEEDS

Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN

Personal Author(s) : WARD, L.K.

Report Date : JUL 1959

Pagination or Media Count : 13

Descriptors :   *AIRFOILS, *SUPERSONIC FLOW, FLUTTER.

Distribution Statement : APPROVED FOR PUBLIC RELEASE