DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE
P. E. Trazzi
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Mach 5 inlet CFD and experimental results [PDF]
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
EFFECT OF FUEL PROPERTIES ON LINER TEMPERATURES IN A SINGLE TUBULAR TURBOJET COMBUSTOR
H. F. Butze
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Nuclear JT11D-20 Turbojet Engine Estimated Performance 1800F NaK Radiator
J. W. Larson
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Simulation of aircraft flights with turbulence and icing conditions. [PDF]
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]
Kittelson DB +25 more
europepmc +1 more source
Summary of investigations of engine response to distorted inlet conditions [PDF]
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
İHA larda İtki İçin Kullanılan Mikro Turbojet Motorun Hava Kompresörünün Termodinamik Analizi
Ali İSMAYİLLİ, Mahmut Sami Büker
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Characterizing and Predicting nvPM Size Distributions for Aviation Emission Inventories and Environmental Impact. [PDF]
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]
Xie Z +10 more
europepmc +1 more source

