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Accession Number:
AD0210613
Title:
THE COMPUTED INSTANTANEOUS VELOCITIES INDUCED AT THE BLADE AXES BY THE SKEWED HELICAL VORTICLES IN THE WAKE OF A LIFTING ROTOR IN FORWARD FLIGHT
Descriptive Note:
Corporate Author:
GEORGIA INST OF TECH ATLANTA
Report Date:
1959-03-01
Pagination or Media Count:
1.0
Abstract:
Distribution Statement:
APPROVED FOR PUBLIC RELEASE