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

Report Date:

1960-05-01

Pagination or Media Count:

1.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE