10. DeSanti (“A Model for Predicting Aircraft Altitude Loss in a Pull-Up from
a Dive,” SIAM Review, 30 (4), pp. 625 – 628, 1988) develops the following
relationship for the ratio between the final velocity, Vf, and the initial velocity,
V0, for an aircraft executing a pull-up from a dive:
1
3Vf
V03
−BVf
V0
−1
3+Bcos γ0= 0.
γ0is the initial flight path angle and B=g/(kV 2
0), where gis the acceleration
due to gravity and kis related to the coefficient of lift. The altitude loss during
the pull-up can be determined from the ratio Vf/V0using the equation
∆y=1−(Vf/V0)2
2kB .
Determine the altitude loss associated with each of the following sets of system
parameters (take g= 9.8 m/s2):
(a) V0= 100 m/s, γ0=−30◦,k= 0.00196 m−1
(b) V0= 150 m/s, γ0=−10◦,k= 0.00145 m−1
(c) V0= 200 m/s, γ0=−45◦,k= 0.00128 m−1
(d) V0= 250 m/s, γ0=−30◦,k= 0.00112 m−1
(a) Let V0= 100 m/s, γ0=−30◦and k= 0.00196 m−1. Then
Using Laguerre’s method with an initial approximation of x0= 0 and a con-
(b) Let V0= 150 m/s, γ0=−10◦and k= 0.00145 m−1. Then