TY - GEN
T1 - Observability of Initial States in One-Dimensional Inviscid Flows With Shocks
AU - Ke, Guanguan
AU - Grauer, Samuel J.
AU - Zaki, Tamer A.
N1 - Publisher Copyright:
© 2026, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2026
Y1 - 2026
N2 - We investigate the observability of initial states in one-dimensional, compressible, inviscid flows with shocks using two-dimensional variational (2DVar) data assimilation and sparse pressure measurements. The Sod shock tube problem is used as a test case, sustaining a canonical wave structure with a shock wave, contact discontinuity, and rarefaction fan. To characterize sensitivity pathways from observations of pressure to the initial state, we analyze adjoint dynamics along acoustic and entropic characteristics in the shock tube and compute initial-time adjoint fields. These fields are assembled to form an observation Jacobian at optimality, which enables a decomposition of state space into linearly observable and unobservable modes. Full-state reconstruction experiments demonstrate that 2DVar reliably reduces errors in the observable directions, while components in the null space persist, reflecting a multiplicity of initial states that are mutually consistent with sparse pressure measurements. An alternative, low-dimensional parameterization of the initial state, based on uniform driver and driven gas states, yields robust reconstructions, and the posterior covariance of the estimated parameters is accurately predicted, up to a scale factor, by the Cramér–Rao bound associated with the reduced-order observation Jacobian. These results may inform the design of control vectors and measurement arrays for data assimilation in shock-dominated flows.
AB - We investigate the observability of initial states in one-dimensional, compressible, inviscid flows with shocks using two-dimensional variational (2DVar) data assimilation and sparse pressure measurements. The Sod shock tube problem is used as a test case, sustaining a canonical wave structure with a shock wave, contact discontinuity, and rarefaction fan. To characterize sensitivity pathways from observations of pressure to the initial state, we analyze adjoint dynamics along acoustic and entropic characteristics in the shock tube and compute initial-time adjoint fields. These fields are assembled to form an observation Jacobian at optimality, which enables a decomposition of state space into linearly observable and unobservable modes. Full-state reconstruction experiments demonstrate that 2DVar reliably reduces errors in the observable directions, while components in the null space persist, reflecting a multiplicity of initial states that are mutually consistent with sparse pressure measurements. An alternative, low-dimensional parameterization of the initial state, based on uniform driver and driven gas states, yields robust reconstructions, and the posterior covariance of the estimated parameters is accurately predicted, up to a scale factor, by the Cramér–Rao bound associated with the reduced-order observation Jacobian. These results may inform the design of control vectors and measurement arrays for data assimilation in shock-dominated flows.
UR - https://www.scopus.com/pages/publications/105031186136
UR - https://www.scopus.com/pages/publications/105031186136#tab=citedBy
U2 - 10.2514/6.2026-0493
DO - 10.2514/6.2026-0493
M3 - Conference contribution
AN - SCOPUS:105031186136
SN - 9781624107658
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
Y2 - 12 January 2026 through 16 January 2026
ER -