Accession Number:

AD0142225

Title:

Transonic Flutter Model Tests. Part III. 60 Degree Delta Wings.

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

• Calcerak, John C.
• Ostaszewski, Nicholas H.

Report Date:

1958-01-01

Pagination or Media Count:

79.0

Abstract:

Descriptors:

• *DELTA WINGS
• *FLUTTER
• TESTS
• TRANSONIC CHARACTERISTICS

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE