Hot Wire Anemometer Measurements in the Unheated Air Flow Tests of the Srb Nozzle-To-Case Joint
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781722280338


Pages:   46
Publication Date:   05 July 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Hot Wire Anemometer Measurements in the Unheated Air Flow Tests of the Srb Nozzle-To-Case Joint


Overview

Hot-Wire Anemometer measurements made in the Solid Rocket Booster (SRB) nozzle-to-case joint are discussed. The study was undertaken to glean additional information on the circumferential flow induced in the SRB nozzle joint and the effect of this flow on the insulation bonding flaws. The tests were conducted on a full-scale, 2-D representation of a 65-in long segment of the SRB nozzle joint, with unheated air as the working fluid. Both the flight Mach number and Reynolds number were matched simultaneously and different pressure gradients imposed along the joint face were investigated. Hot-wire anemometers were used to obtain velocity data for different joint gaps and debond configurations. The procedure adopted for hot-wire calibration and use is outlined and the results from the tests summarized. Ramachandran, N. Unspecified Center NAS8-36474...

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.30cm , Length: 27.90cm
Weight:   0.132kg
ISBN:  

9781722280338


ISBN 10:   1722280336
Pages:   46
Publication Date:   05 July 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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