The relation between spanwise variations in the critical Mach number and spanwise load distributions

Whitcomb, Richard T

NASA NTRS · 19930092722

The relation between spanwise variations in the critical Mach number and spanwise load distributions

Whitcomb, Richard T

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LOAD DISTRIBUTION, WING-SPAN - TAPERED AIRFOILS - BOEING 117 AIRFOILS - NACA 23015-4412 AIRFOILS - NACA 63 (420)-422- 63 (420)-517 LOW-DRAG MACH NUMBER

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Whitcomb, Richard T. 1944-12-01. The relation between spanwise variations in the critical Mach number and spanwise load distributions. https://ntrs.nasa.gov/citations/19930092722

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