Results 211 to 220 of about 763,082 (323)

Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines

, 1955
James Dugan
openalex   +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

Approximate Method for Determining Equilibrium Operation of Compressor Component of Turbojet Engine

, 1955
Merle C Huppert
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

Natural icing of an axial-flow turbojet engine in flight for a single icing condition

, 1948
L. W. Acker
openalex   +1 more source

Investigation of Turbine-outlet Temperature Distribution of XJ34-WE-32 Turbojet Engine

, 1951
William R. Prince, John T Wintler
openalex   +1 more source

Effects of Chevron Nozzles of Small Turbojet Engine on Engine Performance and Jet Noise

, 2018
Gakuyo Tamada, Takuto ISHIKAWA, Toshiaki Tsuchiya   +2 more
openalex   +1 more source

Effects of Altitude on Turbojet Engine Performance

, 1951
William A. Fleming
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