Far-Term Exploration of Advanced Single-Aisle Subsonic Transport Aircraft Concepts [PDF]
Far-term single-aisle class aircraft concepts for potential entry-into-service of 2045 were investigated using an Interactive Reconfigurable Matrix of Alternatives (IRMA) approach.
Blaesser, Nathaniel J. +5 more
core +1 more source
Functional Role of COP1 Gene in Hepatocellular Carcinoma Lipid Metabolism and Stemness
Genes to Cells, Volume 31, Issue 3, May 2026.COP1 promotes HCC lipid metabolism and stemness via the functional interaction with AKR1D1 and TMEM65 genes, respectively, indicating its potential as a therapeutic target for treating primary HCC and preventing metastasis and/or recurrence. ABSTRACT We have previously defined the constitutive photomorphogenic protein 1 (COP1) gene as a therapeutic ...
Eun‐Hye Jeon +8 more
wiley +1 more source
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3 meter transonic cryogenic tunnel [PDF]
Calibration data for the two dimensional test section of the Langley 0.3 Meter Transonic Cryogenic Tunnel were used to develop a Mach number-Reynolds number correlation for the fan pressure ratio in terms of test section conditions.
Adcock, J. B. +2 more
core +1 more source
Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel [PDF]
Static and fluctuating pressure distributions were obtained along the floor of a rectangular-box cavity in an experiment performed in the LaRC 0.3-Meter Transonic Cryogenic Tunnel. The cavity studied was 11.25 in. long and 2.50 in.
Plentovich, E. B., Tracy, M. B.
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Overview of the Applied Aerodynamics Division [PDF]
A major reorganization of the Aeronautics Directorate of the Langley Research Center occurred in early 1989. As a result of this reorganization, the scope of research in the Applied Aeronautics Division is now quite different than that in the past.
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Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers [PDF]
An experiment was performed in the Langley 0.3 meter Transonic Cryogenic Tunnel to study the internal acoustic field generated by rectangular cavities in transonic and subsonic flows and to determine the effect of Reynolds number and angle of yaw on the ...
Chu, Julio +2 more
core +1 more source
Aerodynamic force measurements with a strain-gage balance in a cryogenic wind tunnel [PDF]
Aerodynamic force measurements on a generalized 75 deg delta wing model with sharp leading edges were made with a three component internal strain gage balance in a cryogenic wind tunnel at stagnation temperatures of 300 K, 200 K, and 110 K.
Boyden, R. P. +2 more
core +1 more source
Quadrant swapping technique for partial shaded solar photovoltaic system. [PDF]
Sci RepThangaraj H +4 more
europepmc +1 more source
High Reynolds number tests of the CAST-10-2/DOA 2 transonic airfoil at ambient and cryogenic temper ature conditions [PDF]
The transonic airfoil CAST 10-2/DOA 2 was investigated in several major transonic wind tunnels at Reynolds numbers ranging from Re=1.3 x 10(exp 6) to 45 x 10(exp 6) at ambient and cryogenic temperature conditions.
Demurie, F. +3 more
core +1 more source