Mass Addition Processes in Compressible Flows

The fundamental gas dynamic and thermodynamic effects of simple mass addition in compressible flows are examined. While the driving influences of heat addition and friction in constant area ducts are well understood and commonly taught, relatively little attention is given to the influence of mass addition. These flows are characterized in the same way, increasing the entropy of the flow and driving it to choke at the sonic limit in both supersonic and subsonic cases. Starting from the influence coefficients and continuing previous work, further derivations of thermodynamic gas properties are developed, enabling a comparative analysis between several driving influences. Furthermore, an improvement in the formulation of the streamwise velocity component [Formula: see text] is proposed in order to relate the injection velocity to a fixed reference velocity in place of the variable flow velocity for a range of conditions. This permits the usage of the mass addition driving influence curves in the study of practical systems with injection into compressible flows. Implications of these findings to practical applications in supersonic flows are presented.

Authors

Institutions

Publication Details

Journal
AIAA Journal
Published
2026-10-16
DOI
https://doi.org/10.2514/1.j067029
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Mass Addition Processes in Compressible Flows

Jie Lim, Arthur Paganini, Tonghun Lee
AIAA Journal
Computational Fluid Dynamics and Aerodynamics
article

Mass Addition Processes in Compressible Flows

Jie Lim, Arthur Paganini, Tonghun Lee
article en

Abstract

The fundamental gas dynamic and thermodynamic effects of simple mass addition in compressible flows are examined. While the driving influences of heat addition and friction in constant area ducts are well understood and commonly taught, relatively little attention is given to the influence of mass addition. These flows are characterized in the same way, increasing the entropy of the flow and driving it to choke at the sonic limit in both supersonic and subsonic cases. Starting from the influence coefficients and continuing previous work, further derivations of thermodynamic gas properties are developed, enabling a comparative analysis between several driving influences. Furthermore, an improvement in the formulation of the streamwise velocity component [Formula: see text] is proposed in order to relate the injection velocity to a fixed reference velocity in place of the variable flow velocity for a range of conditions. This permits the usage of the mass addition driving influence curves in the study of practical systems with injection into compressible flows. Implications of these findings to practical applications in supersonic flows are presented.

AIAA Journal
University of Illinois Urbana-Champaign (US), Stanford University (US)
Office of Naval Research, Air Force Office of Scientific Research
Openalex Percentile: Top 19%
Computational Fluid Dynamics and Aerodynamics
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.