Accession Number:
AD0321251
Title:
FLUTTER MODEL TESTS AT HYPERSONIC SPEEDS M EQUALS 5 TO 7
Descriptive Note:
Corporate Author:
CORNELL AERONAUTICAL LAB INC BUFFALO NY
Personal Author(s):
Report Date:
1960-05-01
Pagination or Media Count:
1.0
Abstract:
Descriptors:
Subject Categories:
- Fluid Mechanics