A slat cove filler is utilized to reduce airframe noise resulting from deployment of a leading edge slat of an aircraft wing. The slat cove filler is preferably made of a super elastic shape memory alloy, and the slat cove filler shifts between stowed and deployed shapes as the slat is deployed. The slat cove filler may be configured such that a separate powered actuator is not required to change the shape of the slat cove filler from its deployed shape to its stowed shape and vice-versa. The outer contour of the slat cove filler preferably follows a profile designed to maintain accelerating flow in the gap between the slat cove filler and wing leading edge to provide for noise reduction
One or more acoustic liners comprising internal chambers or passageways that absorb energy from a no...
Acoustic wind tunnel tests were conducted of a wing model with modified leading edge slat and traili...
Noise generated by high-lift devices such as the slats on the leading edge of a wing is a major cont...
Current and new FAA regulations that are to be phased in have begun to pressure the aerospace indust...
Noise produced by unsteady flow around aircraft structures, termed airframe noise, is an important s...
Airframe noise is a growing concern in the vicinity of airports because of population growth and gai...
The leading-edge slat of a high-lift airfoil can be a significant noise contributor during aircraft ...
Airframe noise is a significant component of environmental noise in the vicinity of airports. The no...
Aircraft noise reduction is an application of current intense interest for which smart materials sho...
A multi-element airfoil system includes an airfoil element having a leading edge region and a skin e...
In this study, a slat cove filler (SCF) for a leading-edge slat is designed and its noise and aerody...
In the case of civil transport aircraft, engines were the dominant noise source until the advent of ...
Abstract Noise generated by high-lift devices such as slats on a wing is a major contributor to the ...
The relevance of geometric details to the generation and propagation of noise from leading-edge slat...
Transport class aircraft produce a significant amount of airframe noise during approach and landing ...
One or more acoustic liners comprising internal chambers or passageways that absorb energy from a no...
Acoustic wind tunnel tests were conducted of a wing model with modified leading edge slat and traili...
Noise generated by high-lift devices such as the slats on the leading edge of a wing is a major cont...
Current and new FAA regulations that are to be phased in have begun to pressure the aerospace indust...
Noise produced by unsteady flow around aircraft structures, termed airframe noise, is an important s...
Airframe noise is a growing concern in the vicinity of airports because of population growth and gai...
The leading-edge slat of a high-lift airfoil can be a significant noise contributor during aircraft ...
Airframe noise is a significant component of environmental noise in the vicinity of airports. The no...
Aircraft noise reduction is an application of current intense interest for which smart materials sho...
A multi-element airfoil system includes an airfoil element having a leading edge region and a skin e...
In this study, a slat cove filler (SCF) for a leading-edge slat is designed and its noise and aerody...
In the case of civil transport aircraft, engines were the dominant noise source until the advent of ...
Abstract Noise generated by high-lift devices such as slats on a wing is a major contributor to the ...
The relevance of geometric details to the generation and propagation of noise from leading-edge slat...
Transport class aircraft produce a significant amount of airframe noise during approach and landing ...
One or more acoustic liners comprising internal chambers or passageways that absorb energy from a no...
Acoustic wind tunnel tests were conducted of a wing model with modified leading edge slat and traili...
Noise generated by high-lift devices such as the slats on the leading edge of a wing is a major cont...