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Aerodynamics APPLICATION NOTE Disclaimer Pi Research makes no representation or warranties of any kind whatsoever with
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PROBLEM 2.1 An aircraft has mass of 50 000 kg and a wing area of 210 m2. With the engines giving a thrust of 23.4 kN it
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CONTENT OF STANDARD 4S-10.02 SECTION 1. SCOPE OF SPECIFICATION 2. SUPPLEMENTARY DETAILS SPECIFIED ON DRAWINGS 3. S
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