Some additional information:
Thermoplastic skin we are planning to use comes in RTL solid laminate it has CTE of 3.1/F
Adhesive we are using is fabric type with activation temp around 270F
We are making curved panels about 0.50-0.75" thick and like you said I am trying to come up with appropriate manufacturing process.
Mainly in regards to tooling design, curing cycle and details of the process.
For tooling design/ material: I am focusing on thermal expansion (CTE difference), number of cycles also using thermal stresses to predict life of tool.
Curing cycle: Area needs more research, we started with A cycle but it is causing skin to shift during the curing process as well as core to shift or even break
May be the adhesive we are using is not good or may be we need to add more indexing feature or may be we need to form the curved shape of the skin prior to layup.
Any book/ research material you recommend ?
Note that this is for aircraft interior application
Thanks