Accelerating High-Fidelity Airfoil Design via Physics-Informed Video Diffusion Model. [PDF]
Ai Y +9 more
europepmc +1 more source
ABSTRACT Objective To determine whether myelin‐sensitive quantitative MRI reveals microstructural abnormalities in normal‐appearing cortex (NACtx) in myelin oligodendrocyte glycoprotein antibody–associated disease (MOGAD), indicating that conventional MRI underestimates remission residual cortical injury.
Valentina Camera +20 more
wiley +1 more source
Decoupling pitch and angle of attack with a variable-incidence wing extends quadrotor flight endurance. [PDF]
Shentu C, Niu S, Wang T, Hu J, Wang J.
europepmc +1 more source
Nonlinear flexibility effects on flight dynamics of high-aspect-ratio wings. [PDF]
Tantaroudas ND, Karachalios I.
europepmc +1 more source
Study on wind resistance performance of high-rise corridor building based on quasi-steady static aeroelastic analysis method. [PDF]
Zhang Y.
europepmc +1 more source
Aerodynamic and anatomical changes of the upper airway after maxillary skeletal expansion in adults. [PDF]
Li Z +5 more
europepmc +1 more source
Particle Morphometrics of Glycopyrronium-Formoterol-Budesonide Inhalation Blends Influence Pulmonary Deposition and Bronchodilator Response in Chronic Obstructive Pulmonary Disease (COPD): A Gamma Scintigraphy Study. [PDF]
Jain GK, Mishra A, Chandra N, Madan M.
europepmc +1 more source
Related searches:
The aerodynamic characteristics of cat allergen
Clinical & Experimental Allergy, 1993SummaryTo further characterize airborne cat allergen and a newly established cat challenge facility, airborne Fel d I levels and particle size distributions were studied in both the cat challenge room and home environments under different conditions of ventilation and physical activity.
R A, Wood, A N, Laheri, P A, Eggleston
openaire +2 more sources
Analysis on Aerodynamic Characteristics of a Paraglider Airfoil
Aerotecnica Missili & Spazio, 2016Paraglider sail (canopy) consists of a series of flexible boxes pressurized by special openings located at the leading edge, in the region near to the front stagnation point. Therefore, in order to avoid the deflation of the wing, the pressure inside the sail must remain above a certain threshold.
BOFFADOSSI, MAURIZIO, Savorgnan, F.
openaire +2 more sources

