Generalized indicial forces on deforming rectangular wings in supersonic flight

Harvard Lomax, Franklyn B. Fuller, Loma Sluder
naca-tn-3286
Nov 1954


A method is presented for determining the time-dependent flow over a rectangular wing moving with a supersonic forward speed and undergoing small vertical distortions expressible as polynomials involving spanwise and chordwise distances.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1954/naca-tn-3286.pdf