Numerical Calculation of Effect of Elastic Deformation on Aerodynamic Characteristics of a Rocket

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</svg>-direction deformation of nonspinning rocket body: (a) <svg height="11.175" id="M109" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 11.6625 11.175" width="11.6625" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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q8 -26 43 -107.5t61 -134.5q114 145 174 240q14 24 8 33t-37 13l-34 4l8 28h238z" id="x1D44C"></path></g>
</svg>-direction deformation of nonspinning rocket body at <svg height="11.375" id="M110" style="vertical-align:-0.1638pt" version="1.1" viewbox="0 0 62.0625 11.375" width="62.0625" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> and (b) <svg height="11.175" id="M111" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 11.6625 11.175" width="11.6625" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.062,11.113)"><path d="M667 650l-9 -28q-53 -5 -76 -17t-64 -59q-51 -61 -175 -225q-21 -29 -27 -55l-27 -136q-13 -65 -0.5 -80t83.5 -22l-7 -28h-280l8 28q64 4 81 19t30 83l25 128q6 35 -7 65l-98 231q-17 41 -32.5 52t-68.5 16l8 28h252l-6 -28l-40 -4q-27 -3 -33 -12.5t2 -31.5
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</svg>-direction deformation of nonspinning rocket body at <svg height="13.1375" id="M112" style="vertical-align:-0.1638pt" version="1.1" viewbox="0 0 42.400002 13.1375" width="42.400002" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>.</table>

International Journal of Aerospace Engineering

fig7

Figure 7

Figure 7: Numerical Calculation of Effect of Elastic Deformation on Aerodynamic Characteristics of a Rocket 