Shock tube driver techniques and attenuation measurements,
| Data(s) |
30/12/2024
|
|---|---|
| Resumo |
"Contract AF 18(603)-10, Mechanics Division, Air Force Office of Scientific Research, ARDC, Washington." Mode of access: Internet. |
| Formato |
ren |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Buffalo, Cornell Aeronautical Laboratory, Inc., |
| Direitos |
Items in this record are available as Public Domain, Google-digitized. View access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements. |
| Palavras-Chave | #Fluid dynamics. #Shock waves. #Shock tubes. |
| Tipo |
text |
