Ign, McGraw-Hill,this chapter) and byNew York, 1999, for more information.EXAMPLE 6.18Estimate the landing ground roll distance at sea level for the CJ-1. No thrust reversal= 0. The spoilers increase the zero-lift,used; however, spoilers are employed such that Ldrag coefficient by 10 percent. The fuel tanks are essentially empty, so neglect the wejehrof any fuel carried by the airplane. The maximum lift coefficient, with flaps fully employed at touchdown, is 2.5.

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Answered: of any fuel carried by the airplane.…

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of any fuel carried by the airplane. The maximum lift coefficient, with flaps fully em ployed at touchdown, is 2.5.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

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Fluid Dynamics

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Question

Ign, McGraw-Hill,
this chapter) and by
New York, 1999, for more information.
EXAMPLE 6.18
Estimate the landing ground roll distance at sea level for the CJ-1. No thrust reversal
= 0. The spoilers increase the zero-lift,
used; however, spoilers are employed such that L
drag coefficient by 10 percent. The fuel tanks are essentially empty, so neglect the wejehr
of any fuel carried by the airplane. The maximum lift coefficient, with flaps fully em
ployed at touchdown, is 2.5.

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