General & OtherUniform second-order solution for supersonic flow over delta wing using reverse-flow integral method, by Joseph H. Clarke and James WallaceJ. H. Clarke![Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method, by Joseph H. Clarke and James Wallace]()
Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method, by Joseph H. Clarke and James Wallace
J. H. Clarke
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“Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method, by Joseph H. Clarke and James Wallace” by J. H…
Catalogue details
- Author
- J. H. Clarke
- Category
- General & Other
- Language
- English
- Source
- HathiTrust