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):

• WHITE, RICHARD P. JR.
• KING, STEPHEN R.
• BALCERAK, JOHN C.

Report Date:

1960-05-01

Pagination or Media Count:

1.0

Abstract:

Descriptors:

• *FLUTTER
• *HYPERSONIC CHARACTERISTICS
• *MODEL TESTS
• DAMPING
• EXPERIMENTAL DATA
• FREQUENCY
• MACH NUMBER
• PITCH(MATERIAL)
• PITCH(MOTION)
• STABILITY

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE