Computer-assisted method for estimating stability and time response characteristics of conventional subsonic airplanes

Computer-assisted method for estimating stability and time response characteristics of conventional subsonic airplanes

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3 060 S2R=XR2-SUB 307 0 S3R=XR3-SUB 3080 S4R=0:S4J=0 3090 RETURN 3100 REM quadratic equation solver subroutine based on quadratic eqn. 3110 SJ=C2*C2-4*C3*C1 3120 IF SJ alt; 0 THEN 3180 3130 S1R=(-1*C2+SQR(SJ) )anbsp;...


Title:Computer-assisted method for estimating stability and time response characteristics of conventional subsonic airplanes
Author: Walter von Klein
Publisher: - 1987
ISBN-13:

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