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Accession Number:
ADB806581
Title:
Pressure Distribution on the Fuselage of a Midwing Airplane Model at High Speeds
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC
Report Date:
1943-02-01
Abstract:
Pressure distribution data useful in the structural design of air scoops, vents, and various fuselage parts were obtained in wind-tunnel tests at speeds of 140 to 400 mph at lift coefficients ranging from -0.2 to 1.0. Highest negative pressure on fuselage occurred near the wing. Results indicate that the critical speed of fuselage will be decreased by wing-induced velocities.
Descriptive Note:
Technical note
Pages:
0021
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
0.78MB
