Ornithopter

Ishant dubey

Mohammad Aamir

Abstract –Ā The analysis of the flight of insects, birds andĀ ornithopters is difficult because there is limited aerodynamicĀ theory applicable for the large amplitude, unsteady wingĀ motions. Furthermore, the complex wing shapes and wingĀ motions encountered in insect and bird flight entail complexĀ aerodynamic interactions. A systematic theoretical andĀ experimental study has been pursued by the senior author forĀ the past several years to gain a better understanding of theĀ aerodynamic, dynamic and mechanical problems of flappingĀ wing flight. The primary intent has been to establish a strongĀ technical base necessary for the development of theĀ ornithopter as an alternative to the helicopter. The helicopter isĀ best suited for hovering flight and suffers greatly reducedĀ efficiency as forward speed is increased. On the other hand,Ā the ornithopter can achieve hovering flight, albeit with muchĀ more mechanical complexity, but promises high efficiency inĀ forward flight. The method of attack for this study of theĀ ornithopter has been to depart gradually from the conventionalĀ aircraft configuration so that the large body of knowledgeĀ accumulated in the development of the airplane could beĀ applied to the study of the ornithopter. In this paper, the resultsĀ of the aerodynamic studies have been presented because of theirĀ applicability to the modeling of insect and bird flight.