English, asked by sajidsama0, 6 months ago

The light airplane starts its cruise segment at 82 m/s at 3,000 m when it weighs 1450 kg. After cruising for a period of time at that altitude it is noticed it now weighs 1370 kg. Using a wing area of S = 13.47 m2 compute the final airspeed in (m/s) if the pilot maintains a constant lift coefficient.

Answers

Answered by sanjayranihg
0

Answer:

ye English ka nhi physics ka sawal h beta phor se check kro

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