NASA Technical Reports Server (NTRS) 19800021772: Combined linear theory-impact theory method for analysis and design of high speed configurationsReport as inadecuate



 NASA Technical Reports Server (NTRS) 19800021772: Combined linear theory-impact theory method for analysis and design of high speed configurations


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Pressure distributions on a wing body at Mach 4.63 are calculated. The combined theory is shown to give improved predictions over either linear theory or impact theory alone. The combined theory is also applied in the inverse design mode to calculate optimum camber slopes at Mach 4.63. Comparisons with optimum camber slopes obtained from unmodified

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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