The Problem of Flight: a Text-Book of Aerial Engineering

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Width . 200 ft-.
Speed with no weight .
30 miles per hour Lifting speed (observed) • 36 „ „ Two 20 ft. propellers. Weight of engines 600 lbs. (figs. 16, 59).
Peopessob S. P. Langley's Aerodrome (fig. 60).
Power .....
1-5 H.P.
Weight of engine ....
7 lbs.
Weight of aerodrome . 12 lbs.
Length across planes 14 ft.
Velocity ....
20 miles per hour.
Four rectangular aeroplanes.
Two propellers.
APPENDICES.
105 106 PROBLEM OF FLIGHT.
APPENDIX F.
The Mathematical Theory of the Balloon.
The following ana
...lysis from Dr Glaisher's article on "Aeronautics " in the Encydopcedia Britannica will possibly interest academic students, but it has little practical value, including, as it does, many exceedingly small and uncertain quantities, and not allowing for convective equilibrium.
Let M = mass of balloon, gas, car, and appurtenances.
V„ = capacity of expanded envelope.
v v = volume of gas at atmospheric pressure introduced at starting.
o = volume (less than v ) occupied by same gas at height x p = density of gas in balloon on earth.


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