Accession Number:

AD0255199

Title:

EXPERIMENTAL STUDIES OF FLUTTER OF BUCKLED RECTANGULAR PANELS AT MACH NUMBERS FROM 1.2 TO 3.0 INCLUDING EFFECTS OF PRESSURE DIFFERENTIAL AND OF PANEL WIDTH-LENGTH RATIO

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Personal Author(s):

• SYLVESTER,MAURICE A.

Report Date:

1961-05-01

Pagination or Media Count:

1.0

Abstract:

Descriptors:

• *AIRCRAFT PANELS
• *FLUTTER
• *WINGS
• DEFORMATION
• MODEL TESTS
• PRESSURE
• STRESSES
• SUPERSONIC WIND TUNNELS
• VIBRATION

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE