A shock wave is found to occur behind a driven planar detonation in a shock tube where the piston motion is provided by the contact surface between the detonated and expanding driver gas. Pressure and luminosity records taken in an oxyacetylene mixture, at an initial pressure of 30-50 Torr, show that the secondary shock has similar properties to those predicted by Lee's theory (1965); it is concluded, therefore, that the shock arises because of flow divergence behind the detonation front. Divergent flow in detonations confined in tubes is known to originate through the influence of the wall boundary layer, which effectively causes a negative or outward displacement of the flow boundary. By using this nozzle flow model, which is the basis of velocity deficit theory, measured secondary shock strengths and positions are found to be in agreement with the theoretical predictions over the range of values which are experimentally accessible.