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. The solution for the velocity potential is presented in a form analogous to that for steady supersonic flow having the familiar reflected area concept discovered by Evvard. Particular attention is paid to indicial-type motions and results are expressed in terms of generalized indicial forces.
Generalized Indicial Forces on Deforming Rectangular Wings in Supersonic Flight
1955
31 pages
Report
Keine Angabe
Englisch
Generalized indicial forces on deforming rectangular wings in supersonic flight
Engineering Index Backfile | 1954
|Generalized indicial forces on deforming rectangular wings in supersonic flight
Engineering Index Backfile | 1955
|