Loading…

Pulse Detonation Physiochemical and Exhaust Relaxation Processes

The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significan...

Full description

Saved in:

Bibliographic Details
Main Author:	Schauer, Fred
Format:	Report
Language:	English
Subjects:	CHEMICAL PROPULSION COMBUSTION Combustion and Ignition COMPONENT REPORT DETONATIONS EXHAUST NOZZLES EXHAUST SYSTEMS FUEL AIR RATIO FUELS HYDROCARBONS Jet and Gas Turbine Engines JET ENGINES PDE(PULSE DETONATION ENGINE) PE61102A PE61102F Physical Chemistry PHYSICOCHEMICAL PROPERTIES PROPULSION SYSTEMS PULSE DETONATION ENGINES ROCKET ENGINES SYMPOSIA
Online Access:	Request full text
Tags:	Add Tag No Tags, Be the first to tag this record!

cited_by
cites
container_end_page
container_issue
container_start_page
container_title
container_volume
creator	Schauer, Fred
description	The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significant impact upon performance, will be explored in order to achieve basic understanding of the relationships between detonations, nozzles, and multiple detonation tube interactions. This article is from the ARO-AFOSR Contractors' Meeting (2001) in Chemical Propulsion, p21-23. This article is from ADA401046 Army Research Office and Air Force Office of Scientific Research. Contractors' Meeting in Chemical Propulsion (2001) Held in the University of Southern California on June 18-19, 2001
format	report
fullrecord	<record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADP012098</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADP012098</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADP0120983</originalsourceid><addsrcrecordid>eNrjZHAIKM0pTlVwSS3Jz0ssyczPUwjIqCzOzE_OSM3NTE7MUUjMS1FwrchILC0uUQhKzUmsgKoqyk9OLS5OLeZhYE1LBBrBC6W5GWTcXEOcPXRTSjKT44tLMvNSS-IdXQIMDI0MLC2MCUgDAAPTLtw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Pulse Detonation Physiochemical and Exhaust Relaxation Processes</title><source>DTIC Technical Reports</source><creator>Schauer, Fred</creator><creatorcontrib>Schauer, Fred ; AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH TURBINE ENGINE DIV</creatorcontrib><description>The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significant impact upon performance, will be explored in order to achieve basic understanding of the relationships between detonations, nozzles, and multiple detonation tube interactions. This article is from the ARO-AFOSR Contractors' Meeting (2001) in Chemical Propulsion, p21-23. This article is from ADA401046 Army Research Office and Air Force Office of Scientific Research. Contractors' Meeting in Chemical Propulsion (2001) Held in the University of Southern California on June 18-19, 2001</description><language>eng</language><subject>CHEMICAL PROPULSION ; COMBUSTION ; Combustion and Ignition ; COMPONENT REPORT ; DETONATIONS ; EXHAUST NOZZLES ; EXHAUST SYSTEMS ; FUEL AIR RATIO ; FUELS ; HYDROCARBONS ; Jet and Gas Turbine Engines ; JET ENGINES ; PDE(PULSE DETONATION ENGINE) ; PE61102A ; PE61102F ; Physical Chemistry ; PHYSICOCHEMICAL PROPERTIES ; PROPULSION SYSTEMS ; PULSE DETONATION ENGINES ; ROCKET ENGINES ; SYMPOSIA</subject><creationdate>2001</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27565,27566</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADP012098$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schauer, Fred</creatorcontrib><creatorcontrib>AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH TURBINE ENGINE DIV</creatorcontrib><title>Pulse Detonation Physiochemical and Exhaust Relaxation Processes</title><description>The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significant impact upon performance, will be explored in order to achieve basic understanding of the relationships between detonations, nozzles, and multiple detonation tube interactions. This article is from the ARO-AFOSR Contractors' Meeting (2001) in Chemical Propulsion, p21-23. This article is from ADA401046 Army Research Office and Air Force Office of Scientific Research. Contractors' Meeting in Chemical Propulsion (2001) Held in the University of Southern California on June 18-19, 2001</description><subject>CHEMICAL PROPULSION</subject><subject>COMBUSTION</subject><subject>Combustion and Ignition</subject><subject>COMPONENT REPORT</subject><subject>DETONATIONS</subject><subject>EXHAUST NOZZLES</subject><subject>EXHAUST SYSTEMS</subject><subject>FUEL AIR RATIO</subject><subject>FUELS</subject><subject>HYDROCARBONS</subject><subject>Jet and Gas Turbine Engines</subject><subject>JET ENGINES</subject><subject>PDE(PULSE DETONATION ENGINE)</subject><subject>PE61102A</subject><subject>PE61102F</subject><subject>Physical Chemistry</subject><subject>PHYSICOCHEMICAL PROPERTIES</subject><subject>PROPULSION SYSTEMS</subject><subject>PULSE DETONATION ENGINES</subject><subject>ROCKET ENGINES</subject><subject>SYMPOSIA</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2001</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZHAIKM0pTlVwSS3Jz0ssyczPUwjIqCzOzE_OSM3NTE7MUUjMS1FwrchILC0uUQhKzUmsgKoqyk9OLS5OLeZhYE1LBBrBC6W5GWTcXEOcPXRTSjKT44tLMvNSS-IdXQIMDI0MLC2MCUgDAAPTLtw</recordid><startdate>20010619</startdate><enddate>20010619</enddate><creator>Schauer, Fred</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>20010619</creationdate><title>Pulse Detonation Physiochemical and Exhaust Relaxation Processes</title><author>Schauer, Fred</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADP0120983</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2001</creationdate><topic>CHEMICAL PROPULSION</topic><topic>COMBUSTION</topic><topic>Combustion and Ignition</topic><topic>COMPONENT REPORT</topic><topic>DETONATIONS</topic><topic>EXHAUST NOZZLES</topic><topic>EXHAUST SYSTEMS</topic><topic>FUEL AIR RATIO</topic><topic>FUELS</topic><topic>HYDROCARBONS</topic><topic>Jet and Gas Turbine Engines</topic><topic>JET ENGINES</topic><topic>PDE(PULSE DETONATION ENGINE)</topic><topic>PE61102A</topic><topic>PE61102F</topic><topic>Physical Chemistry</topic><topic>PHYSICOCHEMICAL PROPERTIES</topic><topic>PROPULSION SYSTEMS</topic><topic>PULSE DETONATION ENGINES</topic><topic>ROCKET ENGINES</topic><topic>SYMPOSIA</topic><toplevel>online_resources</toplevel><creatorcontrib>Schauer, Fred</creatorcontrib><creatorcontrib>AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH TURBINE ENGINE DIV</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schauer, Fred</au><aucorp>AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH TURBINE ENGINE DIV</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Pulse Detonation Physiochemical and Exhaust Relaxation Processes</btitle><date>2001-06-19</date><risdate>2001</risdate><abstract>The objective of this program is to establish the scientific knowledge of detonation initiation, propagation, and blow-down needed to develop a pulse detonation engine (PDE) that will operate on hydrocarbon fuels. Detonation tube exhaust blow-down conditions, which are predicted to have a significant impact upon performance, will be explored in order to achieve basic understanding of the relationships between detonations, nozzles, and multiple detonation tube interactions. This article is from the ARO-AFOSR Contractors' Meeting (2001) in Chemical Propulsion, p21-23. This article is from ADA401046 Army Research Office and Air Force Office of Scientific Research. Contractors' Meeting in Chemical Propulsion (2001) Held in the University of Southern California on June 18-19, 2001</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	eng
recordid	cdi_dtic_stinet_ADP012098
source	DTIC Technical Reports
subjects	CHEMICAL PROPULSION COMBUSTION Combustion and Ignition COMPONENT REPORT DETONATIONS EXHAUST NOZZLES EXHAUST SYSTEMS FUEL AIR RATIO FUELS HYDROCARBONS Jet and Gas Turbine Engines JET ENGINES PDE(PULSE DETONATION ENGINE) PE61102A PE61102F Physical Chemistry PHYSICOCHEMICAL PROPERTIES PROPULSION SYSTEMS PULSE DETONATION ENGINES ROCKET ENGINES SYMPOSIA
title	Pulse Detonation Physiochemical and Exhaust Relaxation Processes
url	http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-09T14%3A56%3A45IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Pulse%20Detonation%20Physiochemical%20and%20Exhaust%20Relaxation%20Processes&rft.au=Schauer,%20Fred&rft.aucorp=AIR%20FORCE%20RESEARCH%20LAB%20WRIGHT-PATTERSON%20AFB%20OH%20TURBINE%20ENGINE%20DIV&rft.date=2001-06-19&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADP012098%3C/dtic_1RU%3E%3Cgrp_id%3Ecdi_FETCH-dtic_stinet_ADP0120983%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true