In addition, the choking massflow of swept rotors changes clearly as a result of the spatial change of aerodynamic throat and the forward sweep produces a larger throat area and choking massflow. A noted phenom
The effect of wing sweep on the aerodynamic characteristics of Gurney flaps is examined. Wind tunnel models incorporating un-tapered 2.1 aspect ratio wings with sweeps of 0, 45 and 60 deg were designed and manufactured. Flap heights of 1% and 3% of the chord were evaluated. Testing was undert...
A numerical investigation of the flow evolution over a pitching NACA 0012 airfoil incurring in deep dynamic stall phenomena is presented. The experimental
eep on a wing alone Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing aloneInvestigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone...
of TRACERx are to determine the association between ITH and clinical outcome and the effect of adjuvant platinum-based chemotherapy on ITH in relapsed disease (the latter of which is explored in a companion article9). In 2017, an analysis of the first 100 patients enrolled into TRACERx revealed...
Murray State makes history, Miami returns to the supers on final day of regional action DI Baseball Best individual performances from 2025 NCAA baseball's regionals DI softball FULL 7th inning from thrilling Texas Tech-Oklahoma softball WCWS semifinal ...
In the development of a blended wing body (BWB) planform for low-speed unmanned aerial vehicles (UAV), the present design approach relies on rather cost-effective fidelity tools in aerodynamic modeling and testing. This enables efficient analysis management of the huge parametric studies from airfoi...
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The influence of small attack and sweep angles on the rolling moment variation at a supersonic flow around the bodies close to the bodies of revolution is considered. Based on the method of the differential hypothesis of locality the integral expressions are obtained for the derivatives of the ...
[6] have learned the contributions of tower-induced flow modification toward the uncertainty of the wind resource assessment. On a HAWT with forward and backward swept blades, the effect of the blade sweep direction, the location of the sweep start-up and the tip offset on the aerodynamic ...