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Experimental Effect of Gas Flow Transients on the Heat Release of Burning Liquid Drops in a Rocket Combustor

Heidmann, M. F.

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Experimental Effect of Gas Flow Transients on the Heat Release of Burning Liquid Drops in a Rocket Combustor

Name: Experimental Effect of Gas Flow Transients on the Heat Release of Burning Liquid Drops in a Rocket Combustor
Author: Heidmann, M. F.

Author / Organization: Heidmann, M. F.

Aerospace & Aviation Published 2019 Verification Pending

Overview & Synopsis

Experimental effect of gas flow transients on heat emission of burning liquid drops in a rocket combustor

Indexed from repository: NASA Technical Reports Server (ntrs.nasa.gov)

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Document Title	Experimental Effect of Gas Flow Transients on the Heat Release of Burning Liquid Drops in a Rocket Combustor
Author / Organization	Heidmann, M. F.
Subject & Discipline	OTHER
Categories	Aerospace & Aviation
Publication Year	2019
License / Rights	Public Domain / NASA STI Open Access
Resource Verification	Listed PDF (Verification Pending)
Original Host Website	NASA Technical Reports Server (`ntrs.nasa.gov`)
File Format	application/pdf (Portable Document Format)
Language	EN
Catalog ID	`DOC-68952`
Original Source Link	Visit Source Page on ntrs.nasa.gov »