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Wind-tunnel roll-damping measurements of a winged space shuttle configuration in launch attitude (1973)

Davenport, E. E. ; Hess, R. W.

In: CASI

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Publication Date: 2019-06-27

Description: Ground-wind load studies were conducted on three model configurations to assess the importance of aeroelastic instabilities of erected space shuttle vehicles. Roll damping was measured on a fuselage-alone model, which had a D cross section, and a fuselage and tail surfaces in combination with either a clipped-delta wing or a low-sweep tapered wing as the primary lifting surface. The largest negative roll-damping coefficients were measured with the fuselage-alone configuration and were a function of wind azimuth. At the wind azimuths at which the wing-fuselage configuration was unstable, the negative roll-damping coefficients were a function of reduced frequency.

Keywords: AERODYNAMICS

Type: NASA-TN-D-7394 , L-8991

Format: application/pdf

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