Figure 6.34 shows an increase in specific range with altitude because a. Tr decreases while fuel flow

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Figure 6.34 shows an increase in specific range with altitude because

a. Tr decreases while fuel flow decreases.

b. Tr remains the same while fuel flow decreases.

c. Tr remains the same while Ta decreases.

d. fuel flow remains about the same while airspeed increases.

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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