Buffeting is an aeroelastic phenomenon which plagues high performance aircraft, especially those with twin vertical tails, at high angles of attack. Previous wind-tunnel and flight tests were conducted to characterize the buffet loads on the vertical tails by measuring surface pressures, bending moments, and accelerations. Following these tests, buffeting estimates were computed using the measured buffet pressures and compared to the measured responses. The estimates did not match the measured data because the assumed spatial correlation of the buffet pressures was not correct. A better understanding of the partial (spatial) correlation of the differential buffet pressures on the tail was necessary to improve the buffeting estimates. Severa...
International audienceThe transonic buffet is a complex aerodynamic instability which appears on win...
The predicted upper and lower bounds power spectra for all of the cases and response items given in ...
Buffet onset measurements have been performed on a low13; aspect ratio, moderately swept, aircraft m...
Buffeting is an aeroelastic phenomenon occurring at high angles of attack that plagues high performa...
In 1993, tail buffet tests were performed on a full-scale, production model F/A-18 in the 80 x 120-f...
Tail buffet studies were conducted on a full.scale, production F/A-18 fighter aircraft in the 80 by ...
Tail buffet studies were conducted on a full-scale, production, F/A-18, fighter aircraft in the 80- ...
AbstractThe extension of the aircraft's performance envelope into the high angle of attack regime ca...
Fin buffeting is an aeroelastic phenomenon encountered by high performance aircraft, especially thos...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
The buffeting is a phenomenon that can affect various parts of the aircraft creating problems of str...
The flow around an F/A-18 aircraft at high angle-of-attack is modelled with the aim of predicting th...
The buffeting loads acting on the wing and horizontal tail of a 1/4-scale model of the X-1E airplane...
Wind tunnel tests were carried out on a 1/9th scale model of the F/A-18 at high angles of attack to ...
International audienceThe transonic buffet is a complex aerodynamic instability which appears on win...
The predicted upper and lower bounds power spectra for all of the cases and response items given in ...
Buffet onset measurements have been performed on a low13; aspect ratio, moderately swept, aircraft m...
Buffeting is an aeroelastic phenomenon occurring at high angles of attack that plagues high performa...
In 1993, tail buffet tests were performed on a full-scale, production model F/A-18 in the 80 x 120-f...
Tail buffet studies were conducted on a full.scale, production F/A-18 fighter aircraft in the 80 by ...
Tail buffet studies were conducted on a full-scale, production, F/A-18, fighter aircraft in the 80- ...
AbstractThe extension of the aircraft's performance envelope into the high angle of attack regime ca...
Fin buffeting is an aeroelastic phenomenon encountered by high performance aircraft, especially thos...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
The buffeting is a phenomenon that can affect various parts of the aircraft creating problems of str...
The flow around an F/A-18 aircraft at high angle-of-attack is modelled with the aim of predicting th...
The buffeting loads acting on the wing and horizontal tail of a 1/4-scale model of the X-1E airplane...
Wind tunnel tests were carried out on a 1/9th scale model of the F/A-18 at high angles of attack to ...
International audienceThe transonic buffet is a complex aerodynamic instability which appears on win...
The predicted upper and lower bounds power spectra for all of the cases and response items given in ...
Buffet onset measurements have been performed on a low13; aspect ratio, moderately swept, aircraft m...