Mathur, NB (1999) Estimation of afterbody drag with jet temperature effects for the afterbody-nozzle configuration of a combat aircraft. Journal of Aeronautical Society of India, 51 (3). pp. 181-185.
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Abstract
An empirical correlation developed and validated at NAL (Refs. I and 2) has been utilized to make an estimate of afterbody drag with jet temperature effects from the cold jet tests drag data available for two afterbody-nozzle configurations of a combat aircraft. These results of drag estimates show afterbody drag reduction in the range of 10-25% (With respect to cold jet tests drag results) depending on the operating conditions of the nozzle of the combat aircraft.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Afterbody-nozzle configurations;Combat aircraft;Turbo-jet engine;Turbo-fan engine |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Depositing User: | Ms. Alphones Mary |
| Date Deposited: | 09 May 2006 |
| Last Modified: | 24 May 2010 04:11 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1337 |
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