Abstract: A method for building an aerodynamic structure, an aerodynamic structure, and a vehicle that includes the aerodynamic structure are provided. The method includes providing a structure with at least one substantially-flat exterior surface. The method also includes attaching blocks of rigid fibrous insulation to the at least one substantially-flat outer surface of the structure. Outward-facing surfaces of the blocks of rigid fibrous insulation extend past a target outer mold line of a final aerodynamic shape. The method also includes machining the outward-facing surfaces of the attached blocks to the outer mold line.

Abstract: An integrated pan and spatula system; the integrated pan and spatula system including a cooking vessel and a removably attachable cooking utensil. The cooking utensil includes a handle, a cooking-utensil-head, and cooking-utensil-locking-assembly. The cooking vessel features an inner cooking surface encompassed by a sidewall, a bottom plane including a slot configured to receive the cooking-utensil-head through an open-end of the slot, and a pan-locking-assembly. The pan-locking-assembly and the cooking-utensil-locking-assembly have mating portions and are configured to removably interlock and secure the cooking-utensil-head within the slot of the cooking vessel.

Abstract: A method for building an aerodynamic structure, an aerodynamic structure, and a vehicle that includes the aerodynamic structure are provided. The method includes providing a structure with at least one substantially-flat exterior surface. The method also includes attaching blocks of rigid fibrous insulation to the at least one substantially-flat outer surface of the structure. Outward-facing surfaces of the blocks of rigid fibrous insulation extend past a target outer mold line of a final aerodynamic shape. The method also includes machining the outward-facing surfaces of the attached blocks to the outer mold line.

Abstract: A method for building an aerodynamic structure, an aerodynamic structure, and a vehicle that includes the aerodynamic structure are provided. The method includes providing a structure with at least one substantially-flat exterior surface. The method also includes attaching blocks of rigid fibrous insulation to the at least one substantially-flat outer surface of the structure. Outward-facing surfaces of the blocks of rigid fibrous insulation extend past a target outer mold line of a final aerodynamic shape. The method also includes machining the outward-facing surfaces of the attached blocks to the outer mold line.

Abstract: A method for building an aerodynamic structure, an aerodynamic structure, and a vehicle that includes the aerodynamic structure are provided. The method includes providing a structure with at least one substantially-flat exterior surface. The method also includes attaching blocks of rigid fibrous insulation to the at least one substantially-flat outer surface of the structure. Outward-facing surfaces of the blocks of rigid fibrous insulation extend past a target outer mold line of a final aerodynamic shape. The method also includes machining the outward-facing surfaces of the attached blocks to the outer mold line.

Abstract: Systems and methods for designing oxide ceramic matrix composite parts entail creating a simulation of the oxide ceramic matrix composite part based on expected processing parameters to be used to create the oxide ceramic matrix composite part as well as material characteristics of one or more materials to be used to create the part. The part so created is subjected to simulated structural testing to predict performance of a potential physical counterpart, and the physical counterpart of the simulated oxide ceramic matrix composite part is then produced if the simulated testing yields results that conform to predetermined performance requirements.