Modal Analysis of Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interaction Unsteadiness
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- May 01, 2022
- Source ID
- 10.2514/1.j060880
Entities
People
- Brett F. Bathel
- Christopher S. Combs
- Eugene N. Hoffman
- John D. Schmisseur
- Jose M. Rodriguez
- Joshua M. Weisberger
- Phillip A. Kreth
- Stephanie M. Cottier
- Stephen B. Jones
Organizations
- Air Force Office of Scientific Research
- Langley Research Center
- National Aeronautics and Space Administration
- Office of Naval Research