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NASA NTRS · 19930082282

Two-dimensional unsteady lift problems in supersonic flight

Heaslet, Max A·Lomax, Harvard

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AIR FLOW - AIRFOILS 2-DIMENSIONAL LOADS, GUST - WINGS LOAD DISTRIBUTION - WINGS AIRFOILS - ANGLE OF ATTACK AIR FLOW VELOCITY, HIGH - SUPERSONIC THEORIES - WINGS PRESSURE DISTRIBUTION - AIRFOILS LIFT DISTRIBUTION - WINGS AIR FLOW - AIRFOILS OSCILLATING

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Heaslet, Max A, Lomax, Harvard. 1948-06-01. Two-dimensional unsteady lift problems in supersonic flight. https://ntrs.nasa.gov/citations/19930082282

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