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As a sport flier I've always built my gliders for strength and durability instead of performance (i.e. low weight), which I realize most glider enthusiasts would say is almost a contradiction in terms. So this time I'd like to focus on performance and lower weight.
My immediate thought was using a delta wing planform because of its larger surface area to provide lift, its lower wing loading, and greater strength due to its shape vs traditionally shaped wings. Also a delta wing is naturally stable in pitch so it doesn’t require a separate tail, which further saves weight.
The counter argument is that a delta has more viscous drag compared to a high aspect ratio wing, and swept wings have a better lift to drag ratio, which is why you don't see delta wings in full size conventional aircraft except in supersonic jets, where they have an advantage.
Having said that, at the smaller scale and Reynolds Numbers of BGs and RGs, how much of an advantage or disadvantage would a delta wing have?
My immediate thought was using a delta wing planform because of its larger surface area to provide lift, its lower wing loading, and greater strength due to its shape vs traditionally shaped wings. Also a delta wing is naturally stable in pitch so it doesn’t require a separate tail, which further saves weight.
The counter argument is that a delta has more viscous drag compared to a high aspect ratio wing, and swept wings have a better lift to drag ratio, which is why you don't see delta wings in full size conventional aircraft except in supersonic jets, where they have an advantage.
Having said that, at the smaller scale and Reynolds Numbers of BGs and RGs, how much of an advantage or disadvantage would a delta wing have?