Effect of Chaotic Nature on IPHICLUS and NEARCTIC Flapping MAV Wings in Lift Generation using Welch Power Spectral

Author(s):  
R. Asad Ahmed ◽  
S. Syam Narayanan ◽  
Anandh C.M. Joseph

The application of bio-mimetic in Micro Aerial Vehicles (MAV) is a developing field and has enormous applications in the aviation industry. In this work, experimental investigation of the insect like MAV having flapping wing is discussed. The iphiclus-egensis-aile flexible wing and the nearctic-ceratopogonidae flexible wing were chosen for this study. Values of the coefficient of lift for the unsteady aerodynamics were converted to normalized frequency domain using Welch power spectral density method at various flapping frequencies and Reynolds number. The wing tip vortices were captured using laser visualization technique and further the images were processed using MATLAB. Experimental investigations were carried out in wind tunnel for various velocities and Angle of Attack (AoA) and the results were obtained using digital six component balancing system. Detailed study of both the results shows that the nearctic-ceratopogonidae flexible wing has better lifting properties than the iphiclus-egensis-aile flexible wing at low flapping frequencies and low AoA. For higher flapping frequencies and high AoA, the latter shows better lifting properties than the former.

Author(s):  
G. Nakhaie Jazar ◽  
M. Mahinfalah ◽  
M. Rastgaar Aagaah ◽  
N. Mahmoudian

The third stable region of the Mathieu stability chart, surrounded by one π-transition and one 2π-transition curve is investigated. It is known that the solution of Mathieu equation is either periodic or quasi-periodic when its parameters are within stable regions. Periodic responses occur when they are on a “splitting curve”. Splitting curves are within stable regions and are corresponding to coexisting of periodic curves where an instability tongue closes. Distributions of sub and super-harmonics, as well as quasi-periodic solutions are analyzed using power spectral density method.


2001 ◽  
Author(s):  
Lavi Zuhal ◽  
Morteza Gharib
Keyword(s):  

Author(s):  
Frank T. Zurheide ◽  
Matthias Meinke ◽  
Wolfgang Schröder
Keyword(s):  

2007 ◽  
Vol 51 (02) ◽  
pp. 182-186
Author(s):  
Tracie J. Barber

The accurate prediction of ground effect aerodynamics is an important aspect of wing-in-ground (WIG) effect vehicle design. When WIG vehicles operate over water, the deformation of the nonrigid surface beneath the body may affect the aerodynamic performance of the craft. The likely surface deformation has been considered from a theoretical and numerical position. Both two-dimensional and three-dimensional cases have been considered, and results show that any deformation occurring on the water surface is likely to be caused by the wing tip vortices rather than an increased pressure distribution beneath the wing.


1957 ◽  
Vol 37 (2) ◽  
pp. 85-96 ◽  
Author(s):  
J. J. Sexsmith ◽  
D. T. Anderson ◽  
G. C. Russell ◽  
W. W. Hopewell ◽  
H. Hurtig

Assessments were made of the physical properties of spray deposits from upwind and crosswind, single and multiple flight applications of oil-carrier spray applied by a small aircraft equipped for commercial weed spraying. Volume deposits were determined colorimetrically on petri dish collections of the dyed spray. Droplet assessment data were obtained from photographic enlargement of printflex sampling cards.Three peaks of spray deposit were found, resulting from the propeller blast and the wing-tip vortices. A greater percentage of spray was recovered at ground level, and more variation in volume deposit and droplet size occurred across the effective spray swath, in the upwind flight than in the crosswind flight application. Information obtained from these tests will be used in the construction of a spray booth, designed to apply simulated aerial sprays on a practical small-plot basis, for determining the causes of injury to grain crops resulting from aerial application of herbicide-oil mixtures.


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