Girija, G and Parameswaran, V and Raol, JR (1991) Determination of aircraft performance from flight data. In: National Seminar on quot;Flight Testingquot;, 26-27 Apr 1991, ASTE, Bangalore.
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Abstract
Determination of aircraft performance parameters is an important step in the development and evaluation of modern aircraft.13; The drag polar estimation of the aircraft covering its full envelope was usually performed by 'aircraft acceleration methodsx2019; such as the total energy method for steady state flight and accelerometer method for dynamic maneuver quality. In this paper we describe various special dynamic maneuvers which can be used to extract these parameters to be used for estimation of aircraft performance.13;
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Uncontrolled Keywords: | Flight testing;Angle of attack;Aircraft performance;Flight data |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 06 Feb 2008 |
| Last Modified: | 17 Jun 2010 09:59 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4523 |
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