Readfeed

A. B. Blair

  • Keys to a Happy and Stable FamilyKeys to a Happy and Stable Family
  • Morphing of EvilMorphing of Evil
  • An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speedsAn experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds
  • Effect of tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbersEffect of tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
  • Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speedsEffect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
  • Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbersEffect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
  • Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plateSupersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
  • Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail finsWind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins
  • Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque systemWind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
  • Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll controlWind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control