1. Implementation and Benefits of Variable Geometry Wings for a Supersonic Business Jet
2. Structural Considerations for Variable Sweep Wings
3. AEROELASTIC CHALLENGES FOR A HIGH SPEED CIVIL TRANSPORT
4. Beissner, F.L., Lovell, W.A., Robins, A.W. and Swanson, E.E. "Application of Near-Term Technology to a Mach 2.0 Variable-Sweep-Wing, Supersonic-CruiseExecutiveJet",NASA-CR-172321,1984.
5. Paget,F.M."MechanicalAspectsofVariableSweepWings",SAE670882,SocietyofAutomotiveEngineers,1967.