The feasibility of a one-passenger VTOL (vertical takeoff and landing) craft is under | StudySoup

Textbook Solutions for Engineering Mechanics

Chapter 4 Problem 4/59

Question

The feasibility of a one-passenger VTOL (vertical takeoff and landing) craft is under review. The preliminary design calls for a small engine with a high power-to-weight ratio driving an air pump that draws in air through the 70 ducts with an inlet velocity v 40 m/s at a static gage pressure of 1.8 kPa across the inlet areas totaling 0.1320 m2 . The air is exhausted vertically down with a velocity u 420 m/s. For a 90-kg passenger, calculate the maximum net mass m of the machine for which it can take off and hover. (See Table D/1 for air density.) 4/59

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The first step in solving 4 problem number 59 trying to solve the problem we have to refer to the textbook question: The feasibility of a one-passenger VTOL (vertical takeoff and landing) craft is under review. The preliminary design calls for a small engine with a high power-to-weight ratio driving an air pump that draws in air through the 70 ducts with an inlet velocity v 40 m/s at a static gage pressure of 1.8 kPa across the inlet areas totaling 0.1320 m2 . The air is exhausted vertically down with a velocity u 420 m/s. For a 90-kg passenger, calculate the maximum net mass m of the machine for which it can take off and hover. (See Table D/1 for air density.) 4/59
From the textbook chapter Kinetics of Systems of Particles you will find a few key concepts needed to solve this.

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Title Engineering Mechanics 7 
Author James L. Meriam, L. G. Kraige
ISBN 9780470614815

The feasibility of a one-passenger VTOL (vertical takeoff and landing) craft is under

Chapter 4 textbook questions

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