Andre Weiner, Richard Semaan
					TU Braunschweig, Institute of Fluid
							Mechanics
					
				
Slice of local Mach number $Ma$; $Re_\infty=10^7$, $Ma_\infty=0.75$, $\alpha=4^\circ$.
Unsteady flow and interaction phenomena at high speed stall conditions
 
				Improved understanding and prediction of flight envelop via:
Modal decomp. = spatial structures + temp. behavior
spatial mode
temporal coefficient
Common issues/questions in DMD analyses:
$\rightarrow$ (partial) answers in this presentation
Simulation approach in a nutshell:
 
					Various views of the computational mesh.
Degrees of freedom in DMD analysis:
 
					DMD as a five-step analysis - part I.
 
					DMD as a five-step analysis - part II.
Abbreviations:
opt. TDMD, int. $\rightarrow$ total least-squares DMD with optimal amplitudes and integral mode selection.
Test 0: variance of state vector norms
Test 1: rank sensitivity of buffet frequency
Assumption: top mode = buffet mode
 
				 
				 
				Test 2: sensitivity to the sampling rate
 
				Test 3: rank sensitivity of the full spectrum
 
				 
				Winning configuration:
 
						Temporal mean, std., and probe locations.
PSD based on speed at probe locations.
DMD spectrum obtained from slice data.
 
					Characteristic DMD modes: shock motion and vortex shedding/acoustic waves.
Mode with vortex shedding and acoustic waves.
 
					Comparable modes and spectra for volume, slice, and surface data.
