The Stealth Biplane: a Proposal in Response to a Low Reynolds Number Station Keeping Mission [PDF]
The Stealth Biplane is conceived and constructed to serve as a remotely piloted vehicle designed to navigate a low-level figure-eight course at a target Reynolds number of 100,000.
Donovan, Steven +6 more
core +1 more source
Flow Control Methods and Their Applicability in Low-Reynolds-Number Centrifugal Compressors—A Review
, 2017 The decrease in the performance of centrifugal compressors operating at low Reynolds numbers (e.g., unmanned aerial vehicles at high altitudes or small turbomachines) can reach 10% due to increased friction.
Jonna Tiainen +3 more
semanticscholar +1 more source
Transit Time Theory for a Droplet Passing through a Slit in Pressure-Driven Low Reynolds Number Flows. [PDF]
Micromachines (Basel), 2023 Borbas SW +5 more
europepmc +1 more source
Aerodynamic study of the corrugated airfoil at ultra-low Reynolds number
Advances in Mechanical Engineering, 2019 In this study, Aeshna cyanea dragonfly forewing mid-cross-section corrugated airfoil was simulated at ultra-low Reynolds number. The corrugated airfoil was compared with its smooth counterpart to study the effect of the corrugations upon the aerodynamic ...
Mahmoud E Abd El-Latief +2 more
doaj +1 more source
, 2002 We generalize an analogy between rotating and stratified shear flows. This analogy is summarized in Table 1. We use this analogy in the unstable case (centrifugally unstable flow v.s.
Dubrulle, B., Hersant, F.
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The Harmonic Pitching NACA 0018 Airfoil in Low Reynolds Number Flow
EnergiesThis study investigates the aerodynamic performance of a symmetric NACA 0018 airfoil under harmonic pitching motions at low Reynolds numbers, a regime characterized by the presence of laminar separation bubbles and their impact on aerodynamic forces. The
Jan Michna +2 more
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Effect of Gurney Flaps on Non-Planar Wings at Low Reynolds Number
AerospaceThe effect of spanwise wing non-planarity, employed in conjunction with a Gurney flap, is presented. Testing was undertaken in a low-speed wind tunnel using a rectangular wing with an aspect ratio of three. The outer one-third of the wing was non-planar,
Lance W. Traub
doaj +1 more source
Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Re-Attachment Along the Suction Surface of a Low Pressure Turbine Blade [PDF]
, 2005 B Rk +2 more
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Low Reynolds Number Effect on Highly Loaded Compressor Stator Cascade [PDF]
, 2023 Arun Joseph +3 more
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