Add to ORKGThe design of wing leading edges are primarily based on certification requirements as defined by the regulatory for bird strikes. A typical wing leading edge comprises of skin, rib and baffle plate. The idea of a baffle plate is that it will prevent the bird from impacting the spar, in case of penetration of the skin. The selection of right materials, configuration and fasteners play an important role in containing the damage due to bird strike. The selection of the skin thickness was done based on the RAE empirical formula and through limited bird strike tests on plain leading edge specimens. The role of baffle and selection of its thickness were based on bird strike FE analysis. The selection of fasteners was done based on a rivet pull th...
The Flying-V aircraft concept promises better fuel-burn performance over conventional tube-and-wing ...
In this paper, a parametric numerical study is performed on the sandwich composite leading edge to a...
This paper aims to investigate the crashworthiness capability of a commercial aircraft metallic sand...
The design of wing leading edges are primarily based on certification requirements as defined by the...
Aircraft structures, likely to be subjected to bird strike, have to satisfy a series of requirements...
The work aims to investigate the capability of a vertical tail leading edge to withstand bird strike...
This paper describes an experimental and numerical campaign aimed at assessing the bird strike resis...
Bird-strike is a potentially serious and damaging event for the leading edges of aircrafts. The lead...
This paper aims to investigate the crashworthiness capability of a metallic sandwich leading edge of...
Aircraft leading edges must be certified for a proven level of bird impact resistance. In particular...
Bird strike is a significant design criterion for leading edges of wing and empennage structures. Th...
Abstract The wing leading edge is one of the aircraft structures which are vulnerable to birdstrike....
This paper aims to investigate the crashworthiness capability of a commercial aircraft metallic sand...
Several configuration of a one-bay component of a typical wing leading edge was prepared and tested ...
Click on the DOI link to access the article (may not be free).With the increase in air travel, the r...
The Flying-V aircraft concept promises better fuel-burn performance over conventional tube-and-wing ...
In this paper, a parametric numerical study is performed on the sandwich composite leading edge to a...
This paper aims to investigate the crashworthiness capability of a commercial aircraft metallic sand...
The design of wing leading edges are primarily based on certification requirements as defined by the...
Aircraft structures, likely to be subjected to bird strike, have to satisfy a series of requirements...
The work aims to investigate the capability of a vertical tail leading edge to withstand bird strike...
This paper describes an experimental and numerical campaign aimed at assessing the bird strike resis...
Bird-strike is a potentially serious and damaging event for the leading edges of aircrafts. The lead...
This paper aims to investigate the crashworthiness capability of a metallic sandwich leading edge of...
Aircraft leading edges must be certified for a proven level of bird impact resistance. In particular...
Bird strike is a significant design criterion for leading edges of wing and empennage structures. Th...
Abstract The wing leading edge is one of the aircraft structures which are vulnerable to birdstrike....
This paper aims to investigate the crashworthiness capability of a commercial aircraft metallic sand...
Several configuration of a one-bay component of a typical wing leading edge was prepared and tested ...
Click on the DOI link to access the article (may not be free).With the increase in air travel, the r...
The Flying-V aircraft concept promises better fuel-burn performance over conventional tube-and-wing ...
In this paper, a parametric numerical study is performed on the sandwich composite leading edge to a...
This paper aims to investigate the crashworthiness capability of a commercial aircraft metallic sand...