26- The vehicle sports twin-fuselages made of fiberglass and carbon fiber which are connected by a canard in the front, an airfoil in the middle and a horizontal stabilizer.
27- Based on the piston theory of supersonic flow, the second lagrange equation is used to set up the dynamic equations of an airfoil with store in the supersonic or hypersonic flow.
28- A supporting surface of an airplane ; an airfoil or a wing.
29- The vehicle sports twin-fuselages made of fiberglass and carbon fiber which are connected by a canard in the front, an airfoil in the middle and a horizontal stabilizer.
30- In the method, such an airfoil is termed a four - segment airfoil.
31- The spoiler moving relative to a stationary airfoil is treated by a dynamic overset grid method. The mechanism of the adverse lift because of the rapidly deploying spoiler is analyzed.
32- The transonic flow field around NACA 0012 airfoil is calculated by finite element method from pressure minimum integration(sentence dictionary), full potential equation being used.
33- The experimental results of NACA 0012 airfoil dynamic pressure measurement are given here.
34- The flight mechanism of birds and big insects was probed valuably, and airframe dynamics and airfoil aerodynamics of Flapping Wing Micro Aerial Vehicle (FWMAV) were researched.
35- The properties of bifurcation points of airfoil flutter with cubic nonlinearity in incompressible flow are studied.
36- The dynamical equation of a two - dimensional airfoil with polynomial hysteresis nonlinearity is built in incompressible flow.
37- The results indicate that passive control technique can reduce peak Mach number on the surface of the airfoil and reduce the adverse pressure gradient, shock is also weakened.
38- The vehicle sports twin-fuselages made of fiberglass and carbon fiber which are connected by a canard in the front, an airfoil in the middle and a horizontal stabilizer.
39- The scattering peak of leading edge depends only on radius of airfoil for horizontal polarization.
40- The angle of attack of the high - aspect - ratio wings varies largely as the airflow rounds the airfoil.
41- The high speed airfoil type wind turbine has the highest efficiency in high wind speeds.
42- Lastly, the paper programs to simulate FRP airfoil FW moulding by VC ++.
43- The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
44- Experimentally, the flow-field roud the S-shaped airfoil is tested by means of a water cave.
45- This paper also presents the experimental results of effects of the blade tip clearance and the airfoil shape on the stall flutter boundary.
46- The numerical algorithm is applied for flow over an NACA 0012 airfoil with satisfactory effect.
47- The high speed airfoil type wind turbine has the highest efficiency in high wind speeds.
48- The ejecting flying toy also comprises an afterbody form finalizing sheet which is fixed at the center of the rear part of the airfoil.(30) A numerical method is given to calculate the unsteady lift, pitching moment and drag acting on an airfoil of rotors under attached-flow conditions in a compressible flow.
49- The tutorial begins with a simple four - segment airfoil.
50- Inconel alloy spindle-vane with trenching machined into the airfoil surface to allow for instrumentation wiring.
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