Simulated hailstone tests on windshield materials, on nonmetallic materials used in constructing radar housing in nose of airplane fuselage, on metallic leading edge of wings, and on propeller dome; compressed air catapult projects ice spheres ranging from 0.75 to 1.88 in. in diam, at velocities up to 804 mph.
Hailstone impact tests on aircraft structural components
U S Civ Aeronautics Administration -- Tech Development Report
1950
20 pages
Illustrations, Diagrams, Charts, Tables
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
AIAA | 1972
|NTRS | 1972
|Development of a Hailstone Substitute for Representative Impact Tests
SAE Technical Papers | 2019
|Development of a Hailstone Substitute for Representative Impact Tests
British Library Conference Proceedings | 2019
|Springer Verlag | 2025
|