A NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON
Material type:
TextPublication details: Nasa, Washington, D.C. 1961Description: 55DDC classification: - NASA TR R-85
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TR R-85 (Browse shelf(Opens below)) | Not for loan | TR14358 |
Total holds: 0
Bound With Nasa Tr R-81-84,86-90
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