A platform for an airfoil in a gas turbine engine is provided. The platform includes a top wall configured to connect to an airfoil of the gas turbine engine, a connector configured to receive a pin and secure the platform to a rotor of the gas turbine engine, and a sidewall extending from the top wall to the connector, the sidewall having a first arm and a second arm, wherein the first arm and the second arm are curved such at a bowed sidewall extends from the top wall to the connector.