Unmeel B. Mehta

• A two-stage-to-orbit spaceplane concept with growth potential
• Air-breathing aerospace plane development essential
• Relative advantages of thin-layer Navier-Stokes and interactive boundary-layer procedures
• Some aspects of vortex flows determined from the thin-layer Navier-Stokes equations
• Synthesis of contributed simulations for OREX test cases
• The aerospace plane design challenge
• The computation of flow past an oblique wing using the thin-layer Navier-Stokes equations