Intake Flow Analysis of a Pulsed Detonation Engine

Author:

Strafaccia Joshua A.1,Ölçmen Semih M.2,Hoke John L.3,Paxson Daniel E.4

Affiliation:

1. USAF Test Pilot School Class 15A, 220 South Wolfe Avenue, Edwards AFB, CA 93524; University of Alabama, Tuscaloosa, AL 35487 e-mail:

2. Associate Professor Mem. ASME Aerospace Engineering and Mechanics Department, University of Alabama, Tuscaloosa, AL 35487 e-mail:

3. Innovative Scientific Solutions, Inc., Dayton, OH 45459 e-mail:

4. NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135 e-mail:

Abstract

Unsteady flow within the intake system of a hydrogen–air pulse detonation engine (PDE) has been analyzed using a quasi-one-dimensional (Q1D) computational fluid dynamic (CFD) code. The analysis provides insight into the unsteady nature of localized equivalence ratios and their effects on PDE performance. For this purpose, a code originally configured to model the PDE tube proper was modified to include a 6.1 m long intake with a single fuel injector located approximately 3.05 m upstream of the primary intake valve. The results show that constant fuel mass flow rate injection from the injector creates large local variations in equivalence ratio throughout the PDE within a cycle. The effect of fill fraction on the engine performance is better described with the presence of the inlet model. However, the effect of ignition delay is shown to be better predicted with a model without the inlet.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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