Showing 1 - 6 results of 6 for search 'Shabana, Aysha', query time: 0.02s Refine Results
  1. 1
    Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
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  2. 2
    Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66
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  3. 3
    Estimation of stability derivatives in newtonian limit for oscillating cone
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  4. 4
    Effect of semi vertex angle on stability derivatives for an oscillating cone for constant value of specific heat ratio
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  5. 5
    Effect of sweep angle and a half sine wave on roll damping derivative of a Delta Wing
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  6. 6
    Estimation of stiffness derivative of an ogive for specific heat ratio 1.666
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