Drawing depicting some of the proposed modifications using F-106A 56-0467 as a model to study the installation effects on turbojet exhaust nozzles in the transonic speed range. [NASA via Earle Boyer collection]
Drawing depicting some of the proposed modifications using F-106A 56-0467 as a model to study the installation effects on turbojet exhaust nozzles in the transonic speed range. [NASA via Earle Boyer collection]