Numerical Investigation of the Flow Angularity Effects of the NASA Langley UPWT on the Ares I DAC1 0.01-Scale Model
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
2011-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2011
|ARES I AERODYNAMIC TESTING AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL
British Library Conference Proceedings | 2011
|NTRS | 1999