angle of attack

Another potential advantage results from the fact that the plane is already tilted to a large angle of attack as it rolls down the runway.

If you were a marketing manager, return to the job with a new angle of attack that can help make the company more competitive.

the center of gravity should be located between the aerodynamic center of height and angle of attack and close to the center of height.

ANGLE OF ATTACK, The angle of the wing chord in relation to the free stream airflow as it moves forward through the air.

The hinge moment coefficient breaks before the stall of angle of attack and can be used for predicting stall more safely.

Many of these flights demonstrated the tremendous high angle of attack capabilities of the aircraft.

A sliding mode observer is designed to estimate the angle of attack and flight path angle for a hypersonic vehicle.

The conventional tail must be at a negative angle of attack , and the Canard tail at a positive angle .

It indicated a mismatch in the lower-level comparison in the air data system, specifically with angle of attack.

Once the aircraft airborne there will be a very large angle of attack and the airspeed will decreased rapidly.

The effects of flapping frequency, wind velocity, angle of attack, plane shape of wing and cambered aerofoil are investigated.

the initial stage in application of fuzzy logic to aircraft high-angle-of attack aerodynamics using wind tunnel test data is outlined.

the steady laminar flow field of a hypersonic sharp cone boundary layer with zero angle of attack was computed.

In this paper, the forced rolling movement about the symmetry axis at a fixed angle of attack is numerically simulated.

With the further rising of angle of attack, the area of limit cycles will decrease until limit cycles disappeared.

A zero-install roll angle of the wrap around fins projectile still has roll moment at zero angle of attack.

But, she hopes the suit "will just be one more angle of attack on a really discriminatory policy that is completely un-American. "

State space modeling of unsteady aerodynamics for aircraft at high angle of attack is analyzed here.

The existence of angle of attack reduces the inlet performance.

We performed higher angle of attack maneuvers on Flight 6 as well.

The thermo-flutter of supersonic wing with high angle of attack under the condition of aerodynamic heating was analyzed in this paper.

The research indicated that aircraft can attain agility if maneuver as large angle of attack.

This occurs at one angle of attack for the same wing loading of a paraglider (or any aircraft).

The model of reentry trajectory is established and the angle of attack is regarded as control variable.

As seen above, the design angle of attack for the second segment is10 deg.

Instead of giving up, Mr Obama needs to change his angle of attack.

The results show that: the opposing jet flow is still stable in a small angle of attack, but Mach disk is in the shape of a small tilt;

The Exterior Ballistic Study of Trajectory Correction Shell with Controlled Angle of Attack at the Shell Head

The utility model adopts the differential wheel set, the angle of attack is avoided between a wheel flange and a steel rail;

Investigation of improving the lateral static stability for the aircraft applied to high-subsonic flow and high angle of attack

A study of lateral directional aerodynamic characteristics for combinations at high angle of attack

Experimental research on flow asymmetry of a slender revolutionary body at high angle of attack

An experimental study of pneumatic vortex flow control on high angle of attack forebody model

Research of Integrated Flight and Propulsion Control Design and Simulation for High Angle of Attack Autonomous Approach and Landing

Study of the Optimum Angle of Attack for the Propeller Blade

Experimental Study of the Evolutionary Process of the Flowfield Around Slender Body at High Angle of Attack

First compute the wing's aerodynamic characteristic, get aerodynamic pressure under different angle of attack;

On the Sensitivity of Aircraft Longitudinal Flying Qualities to Aerodynamic Derivatives at High Angle of Attack

Mechanism of Transition in a Hypersonic Sharp Cone Boundary Layer With Zero Angle of Attack

Flutter Analysis of a High-Aspect-Ratio Sandwich Wing under Large Angle of Attack

Study on Identification of Drag Coefficient and Angle of Attack for Unconventional Projectile

An application of the continuous scan technique to the high angle of attack fighter model test

Experiment Investigation of Unsteady Wall Interference to Model Pitching in Large Angle of Attack

Analysis of the Approach Power Compensator System with Constant Angle of Attack

Numerical simulation of turbulence flows about a slender pointed body at high angle of attack

Unsteady N-S Calculations Using a Dual-Time Stepping Method for Airfoils Oscillating at High Angle of Attack

Preliminary research on super-high angle of attack test techniques in a high speed wind tunnel

Investigation of flow field characteristics on a slender body at high angle of attack

Investigation on the interference of rear sting supports at high angle of attack in low speed wind-tunnel

Aerodynamic Modeling of Spatial Maneuvering Aircraft at High Angle of Attack

Numerical Simulation of Flow Field for Wraparound Fins Projectile at Zero Angle of Attack

Research on subsonic wall interference correction for model tests at high angle of attack

Computation of Transonic Turbulent Flow Around a Blunt Nosed Short Body at Large Angle of Attack

Guidance motion model and guidance law design of the angle-of-attack missile

Analyses on the missile's aerodynamic coupling control system with large angle of attack

Analysis of Supersonic Thermo-Flutter of the Wing with High Angle of Attack

Implemental Method of Parameter Simulation for Angle of Attack and Sideslip Signal

The Aerodynamic Ablation of Hypersonic Penetrator Shell at Angle of Attack

The Comparison of Several Unsteady Aerodynamics Models at High Angle of Attack

The Advance of Aircraft Flying Qualities Researching at High Angle of Attack

Study on High-Angle-of-Attack Measurement Method on High Maneuvering Missile

Decoupled Control for a High Angle of Attack Missile Based on Differential Geometry Method

Attitude Control for Large Angle-of-attack of Antiaircraft Missile

Effects of Vortex Generators on Maximum Lift and Stall Angle of Attack over Wings

A neural network based inverse system method for high angle-of-attack control

Study about high angle of attack flying qualities with simulator

Control of Asymmetric Flow Fields of Slender Bodies at High Angle of Attack

Proportional Side Force Control of Slender Body at High Angle of Attack

Boundary Element Analysis on the Flow Field and Pressure Field of Flow around Cascades with Small Angle of Attack

Nonlinear Control Law Design for High Angle of Attack Flight

Study on high angle of attack test technique of rear sting supports

Cut oxygen flow velocity, momentum and Angle of attack;

Angle of Attack's Kalman Filter Estimation in Vertical Gust

angle of attack automatic control system;

Fig. 2 Distribution of lift and angle of attack on the rotor of helicopter

A New Method for Restraining the Angle of Attack

High angle-of-attack control law design based on global stability analysis

angle of attack sensing system

Angle of attack, pitch angle

angle of attack at minimum drag

angle of attack at maximum lift

angle of attack; zero lift

angle of attack at zero lift

angle of attack at stall

Angle of attack of blade

The real-time model angle of attack measurement based on image and it's application in wind tunnel