Given the followingTrim-Diagram answer the questions in the followingtable
Given The Following Trim Diagram Answer The Questions In The Following Table 1 (91.39 KiB) Viewed 26 times
NOTES: 1. Xc.9. AFT Xc.g. FWD 12. SE = 0° +.4 =.540 +.3 3. FLAPS UP + 1 y = -6° = .365 1 Cm=0 FOR X +.2 7 .365 +.1 Cm=0 Xcg= 440 ·1.6 T CL 1.4 1.2 1.0 .8 .6 0 1 -2° -.1 Cm=0 -Xeg. = α .540 0% ·∞ = 14° MAX -α = 7° = 0° -.2 -3 Question 1 Ata = 0, what is the stabilizer angle to trim the aircraft 2 What is the range within which the horizontal Stabilizer is effective to trim the aircraft What is the range of Angle of attack for which the aircraft can be trimmed 4 What is the range of center of gravity for which the aircraft can be trimmed 5 At i = 0, what is the range of a that we can trim the aircraft 6 |At i = 7, what is the range of a that we can trim the aircraft 7 What is the value of C10 Answer
L SE E C₁iH + C₁ C₁... S C₁ = C₁+C₁₂a + СLiH Ή L Lo La
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