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Plane-flame simulation of the wake behind an internally propelled vehicle Part 1, simulation of a supersonic vehicle by a…

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6. References 1. Foa, J.V., IIPropulsion of a Vehicle in a Tube", Rensselaer Polytechnic Institute, TR AE 6404, Troy,…
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28 TABLES AND FIGURES
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TABLE I Results for Inviscid Adiabatic Flow LOCATION U A -f /fa S SLOPE - Tail of Expansion Wave -0.983 2.380 3.410…
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INERT GAS DETONABLE MIXTURE FIGURE 1 Gases at rest before ignition I ) I ~ ~ I ... - ~ SHOCK I INTERFACE…
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T INTERFACE 10 EXPANSION 8 SHOCK DETONATION -16 -8 o 8 16 24 32 40 ~ FIGURE 3 Wave diagram for inviscid…
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T' = 7.5 T'=6 28 24 FIGURE 4 T'=5 T'=4 T'=3 T'=2 T' = 1 20 16 12 8 4 e…
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-/6 INTERFA7 \ \ \ \ \ \ \ \ SHOCK \ -8 \ \ \ \ \ \ \ ~ o T /0 8 6 4 EXPANSION DETONATION 8 16…
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48 I NVISCID ADI ABATIC INTERFACE 40 FIGURE 6 TAIL OF EXPANSION 32 24 ~ FRICTION -HEAT TRANSFER 16 8 Comparison of…
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----------- - - - - - - - - 28 24 FIGURE 7 T = I 20 /6 /2 8 4 Pressure distribution in a coordinate system fixed to…
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r=3 r=2 r=1 r = 7.5 r=5 r ----------------- ~ ~ ~ ~ ~ .~ 28 24 FIGURE 8 20 16 12 8 4 ~ Velocity…
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- - - - - - - - - - - T = 7.5 28 24 FIGURE 9 r = I ,=2 r=3 ,=4 20 16 12 8 4 ! Temperature distribution in a…
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T Sllli 21111 ~ FIGURE 10 Construction of characteristic grid
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\ \ \ \ __ ~v ,...--- I I I , r-l r-l
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T \ \ ~~~ r ,. "'-5 3\ \ t FIGURE 12 Solution for a characteristic crossing an interface
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T e FIGURE 13 Solution for a characteristic crossing a shock

Plane-flame simulation of the wake behind an internally propelled vehicle Part 2, simulation of a supersonic vehicle by a heat…

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PROJECT TUBEFL/OHT
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TR AE 6705 PLANE-FLAME SIMULATION OF THE WAKE BEHIND AN INTERNALLY PROPELLED VEHICLE PART 2 SIMULATION OF A SUBSONIC…
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TABLE OF CONTENTS Page ABSTRACT iv SYMBOLS v 1. INTRODUCTION 2. EQUATIONS OF MOTION 3. RESULTS 4. CONCLUSION 5.…
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ABSTRACT The development of the flow field about an internally-propelled vehicle in steady motion at subsonic speed in a tube…
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SYMBOLS ~ speed of sound A ~ 0... /0..." nondimensional speed of sound ~ specific heat at constant pressure c…
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u:::. u..( d" 1 1 ' 0...0 non ~mens~ona ve oc~ty ~ velocity relative to heat source ~ distance along tube…
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1 I. INTRODUCTION 1 This report presents the second part of a study of the effects of friction and heat transfer on the…
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2 detonation is used to generate a flow field simulating that induced by an internally-propelled supersonic vehicle. In the…
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3 On ignition, a forward-facing shock 1 starts traveling through the mixture while a rearward-facing shock 2 starts…
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and heat transfer. Although idealized, this model is capable of revealing the essential features of dissipation in the flow…
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