AIAA-2001-0531 Direct Calculation of Turbomachinery Flows Using the Space-Time Conservation Element and Solution Element Method
39th, Aerospace sciences meeting ; 2001 ; Reno, NV
2001-01-01
ALL
Paper nos AIAA-2001-0007 to AIAA-2001-0660 with gaps
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Interpolation Methods for Inlet Distortion Determination (AIAA 2016-0531)
British Library Conference Proceedings | 2016
|AIAA 2006-0531 Unstructured Viscous Layer Insertion Using Linear-Elastic Smoothing
British Library Conference Proceedings | 2006
|Design Optimization of a Scramjet Vehicle for Ascent Using Surrogate Optimization (AIAA 2014-0531)
British Library Conference Proceedings | 2014
|