Results 111 to 120 of about 1,472 (179)

Operability of an Ejector Enhanced Pulse Combustor in a Gas Turbine Environment [PDF]

open access: yes
A pressure-gain combustor comprised of a mechanically valved, liquid fueled pulsejet, an ejector, and an enclosing shroud, was coupled to a small automotive turbocharger to form a self-aspirating, thrust producing gas turbine engine.
Dougherty, Kevin, Paxson, Daniel E.
core   +1 more source

NASA Tech Briefs, June 2004 [PDF]

open access: yes
Topics covered include: COTS MEMS Flow-Measurement Probes; Measurement of an Evaporating Drop on a Reflective Substrate; Airplane Ice Detector Based on a Microwave Transmission Line; Microwave/Sonic Apparatus Measures Flow and Density in Pipe; Reducing ...

core   +1 more source

Analytical study of control devices for high amplitude combustion instability Quarterly report [PDF]

open access: yes
Mathematical model and analysis of combustion processes in annular rocket engines for control of high amplitude combustion ...
Burstein, S. Z., Schechter, H.
core   +1 more source

Operational Stability Limits in Rotating Detonation Engine Numerical Simulations [PDF]

open access: yes
An instability is described which arises in computational fluid dynamic (CFD) simulations of semi-idealized rotating detonation engines (RDE) configured with a throat at the exit.
Paxson, Daniel E., Schwer, Douglas A.
core   +1 more source

Applications of aerospace technology in the electric power industry [PDF]

open access: yes
An overview of the electric power industry, selected NASA contributions to progress in the industry, linkages affecting the transfer and diffusion of technology, and, finally, a perspective on technology transfer issues are ...

core   +1 more source

Characterizing acoustic modes in a hollow rotating detonation combustor

open access: yesCombustion and Flame
Tyler Pritschau   +2 more
openaire   +1 more source

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