Static tests of the ada 1/3 scale document no. Aircraft intake model

Chidananda, MS and Jagannatha Rao, B and Venkatesh , S and Krishna Kumar, VS (1988) Static tests of the ada 1/3 scale document no. Aircraft intake model. Project Report. National Aerospace Laboratories, Bangalore.

[img] PDF
PD_PR_8806.pdf - Published Version

Download (66kB)

Abstract

Static tests were carried out on an 1/3 scale aircraft Intake model provided by ada.the tests (subsonic) were Carried out using an ejector developed for the purpose. Due to losses at the intake entrance, it was not possible To draw the required air flow through the intake. Intake Wall static and engine face total pressure distributions Were determined for engine face mach numbers varying from 0.17 to 0.43. The intake performance, including the entrance Effects for the geometry given, has been presented in this Report, as determined under static conditions.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Air intakes, intake ducts, intake performance, static performance, intake flows
Subjects: AERONAUTICS > Aircraft Propulsion and Power
Depositing User: Ms Indrani V
Date Deposited: 24 Aug 2012 10:36
Last Modified: 24 Aug 2012 10:36
URI: http://nal-ir.nal.res.in/id/eprint/10852

Actions (login required)

View Item View Item