NASA NASA-TN-D-6283
NASA NASA-TN-D-6283 1971-JAN-01 A tme-dependent method for calculatng supersonc angle-of-attack flow about axsymmetrc blunt bodes wth sharp shoulders and smooth nonaxsymmetrc blunt bodes
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Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based on time dependent finite difference theory and method of characteristics