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Type of Document	Master's Thesis
Author	Martin, Victor J.
URN	etd-03142005-145716
Persistent URL	http://resolver.caltech.edu/CaltechETD:etd-03142005-145716
Title	Airplane takeoff performance
Degree	Master of Science
Option	Aeronautics
Advisory Committee	Advisor Name Title Unknown Committee Chair
Keywords	none
Date of Defense	1936-01-01
Availability	unrestricted
Abstract In this paper a general equation for calculating the takeoff performance of landplanes is developed in terms of the usual airplane parameters. The analysis enables the ground effect, wind and atmospheric conditions, altitude, and the use of flaps to be taken into account. A simple and rapid method is presented for the determination of the best flap angle to be used for takeoff. Variation in takeoff performance due to changes in any of the airplane or engine-propeller characteristics is readily determined through the introduction of a new takeoff acceleration parameter. A method for calculating the propeller speed, engine power, and thrust variation for both fixed-pitch and constant-speed propellers is included, and a new significance is given to the thrust versus square of velocity curve for takeoff computations. Examples are included to illustrate the use of the analysis in solving the various takeoff problems.
Files	Filename       Size       Approximate Download Time (Hours:Minutes:Seconds)     28.8 Modem   56K Modem   ISDN (64 Kb)   ISDN (128 Kb)   Higher-speed Access    Martin_vj_1936.pdf 3.10 Mb 00:14:21 00:07:23 00:06:27 00:03:13 00:00:16