Results 101 to 110 of about 2,713 (191)

Multi-Disciplinary Optimization of Mixed-Flow Turbine for Additive Manufacturing

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
Additive manufacturing offers new perspectives for creating complex geometries with improved design features at lower cost and with reduced manufacturing time.
Victor Loir   +2 more
doaj   +1 more source

Review of ejector nozzles. Part 2 – Mixers and additional information

open access: yesАвіаційно-космічна техніка та технологія
The subject of this article is ejector nozzles, which are intended for the thrust augmentation of jet engines and their corresponding flow mixers. The goal is to soften the acuteness of contradictions between the required high performance (especially ...
Ruslan Tsukanov, Sergiy Yepifanov
doaj   +1 more source

Increasing returns and network structure in the evolutionary dynamics of industries [PDF]

open access: yes
The paper explores the idea that properties at the level of firms coevolve with more aggregate properties at the level of market institutions in the dynamics of industries.
Andrea Bonaccorsi, Paola Giuri
core  

Combined Methods in Preliminary Micro Scale Gas Turbine Diffuser Design – a Practical Approach

open access: yesJournal of Applied Fluid Mechanics, 2018
Micro scale gas turbines are low cost, simplified versions of full scale jet engines. A unique feature of their design are centrifugal compressor impellers that are selected from automotive low cost, high quality turbocharger components.
M. Czarnecki, J. Olsen
doaj  

Effects of forward velocity on noise for a J85 turbojet engine with multitube suppressor from wind tunnel and flight tests [PDF]

open access: yes
Flight and wind tunnel noise tests were conducted using a J85 turbojet engine as a part of comprehensive programs to obtain an understanding of forward velocity effects on jet exhaust noise.
Miles, J. H.   +2 more
core   +1 more source

On the use of relative velocity exponents for jet engine exhaust noise [PDF]

open access: yes
The effect of flight on jet engine exhaust noise has often been presented in terms of a relative velocity exponent, n, as a function of radiation angle.
Stone, J. R.
core   +1 more source

This is NASA [PDF]

open access: yes, 1965
Mission, facilities, and projects of ...

core   +1 more source

Home - About - Disclaimer - Privacy