Results 161 to 170 of about 14,411 (284)

Mach 5 inlet CFD and experimental results [PDF]

open access: yes
An experimental research program was conducted in the NASA Lewis Research Center 10 x 10 ft supersonic wind tunnel. The 2-D inlet model was designed to study the Mach 3.0 to 5.0 speed range for an over-under turbojet plus ramjet propulsion system.
Reddy, D. R.   +2 more
core   +1 more source

Simulation of aircraft flights with turbulence and icing conditions. [PDF]

open access: yesSci Data
Dampeyrou C   +3 more
europepmc   +1 more source

Experimental verification of principal losses in a regulatory particulate matter emissions sampling system for aircraft turbine engines. [PDF]

open access: yesAerosol Sci Technol, 2021
Kittelson DB   +25 more
europepmc   +1 more source

Summary of investigations of engine response to distorted inlet conditions [PDF]

open access: yes
A survey is presented of experimental and analytical experience of the NASA Lewis Research Center in engine response to inlet temperature and pressure distortions.
Abdelwahab, M.   +3 more
core   +1 more source

Characterizing and Predicting nvPM Size Distributions for Aviation Emission Inventories and Environmental Impact. [PDF]

open access: yesEnviron Sci Technol
Durdina L   +9 more
europepmc   +1 more source

Metabolomic analysis of gut metabolites in patients with colorectal cancer: Association with disease development and outcome. [PDF]

open access: yesOncol Lett, 2023
Xie Z   +10 more
europepmc   +1 more source

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