DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0142225
Title:
Transonic Flutter Model Tests. Part III. 60 Degree Delta Wings.
Descriptive Note:
Corporate Author:
CORNELL AERONAUTICAL LAB INC BUFFALO NY
Report Date:
1958-01-01
Pagination or Media Count:
79.0
Abstract:
Distribution Statement:
APPROVED FOR PUBLIC RELEASE