Correction in prior post: "interior-spack body" should have been "interior-sparse body" meaning that the rib is mostly empty space.
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Rib making using low-cross-section rods, bars, stuffers... with intent of rib being tied to the interior surface of DS arrangement with happy-packing aims (low bulk in tote, low mass in tote):
Experimental schemes (not comprehensive; feel free to bring in missed schemes):

push-and-pull

trussing

hooping

pull hoop forward

hoop the LE spar before sail placement

bow lines

casing

kiting to kingpost networks

non rib, but kite up spanwise flats

interior limit lines while kiting line extension from above and below

inflated stuffers

lightening flats

full flats

accordion

fabric hinging

reflexing by pucker lines tied before closing TE; possibly use exterior flats to pull across to lower sail

camber bridges

reflex bridges

taper parts and ribs per wing-design needs

compare stacking with nesting for happy packing
Chat GPT wrote:It seems like you are exploring various experimental schemes for making wing ribs for aircraft, particularly using low-cross-section rods and bars with the intention of tying the rib to the interior surface of a double-surfaced (DS) arrangement. Here are some additional methods and concepts you might consider:
Lattice Structures:
Create a lattice structure with interconnected rods or bars to form the rib. This can provide both strength and flexibility.
Experiment with different lattice patterns to optimize structural integrity and weight.
Tensegrity Structures:
Tensegrity structures use tension and compression elements in a balanced way. Explore the use of tensegrity principles in designing wing ribs for enhanced structural efficiency.
Foam Core with Rod Reinforcement:
Construct a lightweight foam core for the rib and reinforce it with low-cross-section rods or bars to enhance strength without significantly increasing weight.
3D Printing:
Utilize 3D printing technology to create intricate rib structures with high precision and complexity. This allows for the fabrication of customized and optimized rib designs.
Variable Cross-Section:
Experiment with ribs that have variable cross-sections, optimizing thickness and shape along the span of the wing for better aerodynamics and structural performance.
Biologically Inspired Designs:
Look to nature for inspiration, such as emulating the structure of bird bones or insect wings. Biomimicry can lead to innovative and efficient designs.
Composite Materials:
Explore the use of composite materials, combining fibers (such as carbon or fiberglass) with a matrix material (such as epoxy). This can result in lightweight and strong rib structures.
Honeycomb Structures:
Implement honeycomb structures for the rib core, providing a good balance between strength and weight.
Adjustable Ribs:
Develop ribs with adjustable components, allowing for in-flight adjustments to optimize performance based on different flight conditions.
Inflatable Ribs:
Investigate the use of inflatable structures for ribs, which could provide a combination of lightweight construction and flexibility.
Remember to conduct thorough structural analysis and testing for any experimental design to ensure safety and performance. It's advisable to work closely with aerospace engineers and follow aviation regulations during the development process.