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| Title | Author(s) | Source | Page(s) |
|---|---|---|---|
| Computation of aerodynamic load and coefficient for satellite launch vehicle | Mehta, R C; Sastry, M S | IJEMS Vol.04(2) [April 1997] | 41-48 |
| Thermal stress analysis of a solid rocket motor nozzle throat insert using finite element method | Mehta, R C; Suresh, K; lyer, R Narayana | IJEMS Vol.05(5) [October 1998] | 271-277 |
| Solution of inverse heat conduction problem using explicit and implicit schemes | Mehta, R C; Radhakrishnan, T V; Seetharamu, K N | IJEMS Vol.02(5) [October 1995] | 205-211 |
| Flow structure of a supersonic jet impinging on an axisymmetric deflector | Mehta, R C; Prasad, J K | IJEMS Vol.04(5) [October 1997] | 178-188 |
| Estimation of shock-cell structure of axisymmetric supersonic free jets | Mehta, R C; Prasad, J K | IJEMS Vol.03(4) [August 1996] | 141-147 |
| Phase transformation and residual stress analysis in cryo-treated single point cutting tool | Mehta, R C; Sinha, P P; Asokan, S; Mohanlal, D | IJEMS Vol.02(3) [June 1995] | 95-102 |