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Accession Number:
AD0265481
Title:
TAKE-OFF DISTANCES OF A SUPERSONIC TRANSPORT CONFIGURATION AS AFFECTED BY AIRPLANE ROTATION DURING THE TAKE-OFF RUN
Corporate Author:
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
Report Date:
1961-10-01
Abstract:
An analytical study has been made to determine the effects of rotation speed, rotation angle, and rotation time on the take-off distance of a supersonic transport configuration. The takeoff distances were also determined at various rotation speeds to show the effects of such configuration changes as wing loading, maximum lift coefficient, thrust-weight ratio, and induced drag. Author
Pages:
0001
File Size:
0.00MB
