A fully implicit time accurate method for hypersonic combustion : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.
| Author/creator | Yungster, Shaye |
| Other author | Radhakrishnan, Krishnan. |
| Other author | Lewis Research Center. Institute for Computational Mechanics in Propulsion. |
| Format | Book |
| Publication Info | Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va.] : [National Technical Information Service, distributor], [1994] |
| Description | 1 volume. |
| Series | NASA technical memorandum ; 106707 NASA technical memorandum 106707. ^A467613 |
| General note | Distributed to depository libraries in microfiche. |
| General note | Shipping list no.: 95-0744-M. |
| Reproduction note | Joyner- Microfiche. [Washington, D.C. : Supt. of Docs., U.S. G.P.O., 1995] 1 microfiche. |
| GPO item number | 0830-D (MF) |
| Govt. docs number | NAS 1.15:106707 |