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Accession Number:
AD0489862
Title:
SUPPLEMENTARY STUDY REPORT ROTOR/WING CONCEPT STUDY
Corporate Author:
HUGHES TOOL CO CULVER CITY CA AIRCRAFT DIV
Report Date:
1966-02-01
Abstract:
The basic data and analyses from the RotorWing wind tunnel tests were reported in HTC-AD 65-15 AD-473 862L, 863L, 864L. Supplementary analyses of the data with respect to RotorWing rolling and pitching moments in the low- rpm range, RotorWing shaft bending moments in 1-g running-rotor flight, horizontal tail efficiency, and RotorWing blade root bending moments are included in this report.
Supplementary Note:
DOI: 10.21236/AD0489862
Pages:
0035
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
NONR-4588(00)
File Size:
1.73MB
