Accession Number:

AD0142225

Title:

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

Personal Author(s):

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Report Date:

1958-01-01

Supplementary Note:

Rept. on Aeroelasticity, Vibration and Noise.

Pages:

0079

Descriptors:

Contract Number:

AF33 616 179

File Size:

0.00MB

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