Accession Number:

AD0078081

Title:

EFFECTS OF STRUCTURAL FLEXIBILITY ON GUST LOADING OF AIRCRAFT. PART 2. DYNAMIC STRESSES IN SWEPT-WING AIRPLANES

Descriptive Note:

Corporate Author:

MASSACHUSETTS INST OF TECH CAMBRIDGE AEROELASTIC AND STRUCTURES RESEARCH LAB

Report Date:

1955-08-01

Pagination or Media Count:

1.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE