Aerospace Engineering > GATE 2022 > Aircraft Stability
Regarding the horizontal tail of a conventional airplane, which one of the following statements is true?
A
It contributes to Cmα < 0
B
It makes Cmα = 0
C
It makes Cmα > 0
D
It makes Cm0 > 0 and Cmα > 0

Correct : a

Similar Questions

For an airplane having directional/weathercock static stability, which of the following options is/are correct?
#56 MSQ
For a general aviation airplane, one of the complex conjugate pairs of eigenvalues for longitudinal dynamics is given by -0.039 ± 0.0567i (in SI units). If the...
#70 Fill in the Blanks
For a longitudinally statically stable aircraft, which one of the following represents the relationship between the coefficient of pitching moment about the cen...
#92 MCQ

Related Topics

No tags found

Unique Visitor Count

Total Unique Visitors

Loading......