Results 191 to 200 of about 11,681 (284)

Computational Investigation of a Boundary-Layer Ingesting Propulsion System for the Common Research Model. [PDF]

J Aircr, 2019
Blumenthal BT, Elmiligui AA, Geiselhart KA, Campbell RL, Maughmer MD, Schmitz S.   +5 more
europepmc   +1 more source

Thrust augmentation for a small turbojet engine

, 1999
A Sophia J450 (nine pounds of thrust) gas turbine engine was used first to examine the thrust augmentation generated using an ejector shroud. Experimental results obtained with and without the ejector were compared with performance predicted using an engine code and a one-dimensional ejector analysis. The engine code was revised to incorporate a radial
openaire   +1 more source

Design and Experimental Study of an Over-Under TBCC Exhaust System. [PDF]

J Eng Gas Turbine Power, 2014
Mo J, Xu J, Zhang L.
europepmc   +1 more source

Turbine for a low cost turbojet engine. 1: Design and cold-air performance

, 1974
M. G. Kofskey, R. J. Roelke
openalex   +1 more source

A new bottom-up emissions estimation approach for aircraft sources in support of air quality modelling for community-scale assessments around airports. [PDF]

Int J Environ Pollut, 2019
Arunachalam S, Naess B, Seppanen C, Valencia A, Brandmeyer JE, Venkatram A, Weil J, Isakov V, Barzyk T.   +8 more
europepmc   +1 more source

Effect of Forging Temperature and Heat Treatment on the Performance of Inconel 700 Buckets at 1625 Degrees F in a J33-9 Turbojet Engine

, 1958
C. A. Gyorgak, D F Springsteen, J R Johnson   +2 more
openalex   +1 more source

Nonlinear Dynamic Modeling of Turbojet Engines with Cnn-Lstm Networks

Lei Chen, Dong Wei, Hang Su, Chi Yu, Congling Tian, Yongzhuo Gao, Dongmei Wu, Hui Dong   +7 more
openalex   +1 more source

Opportunities for nanomaterials in more sustainable aviation. [PDF]

Discov Nano
Pendashteh A, Mikhalchan A, Blanco Varela T, Vilatela JJ.   +3 more
europepmc   +1 more source