Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 /
| Data(s) |
07/07/1974
|
|---|---|
| Resumo |
Prepared at Langley Research Center. Cover title. Includes bibliographical references (p. 17-19). Mode of access: Internet. |
| Formato |
bib |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], |
| 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 | #Cylinders. #Drag (Aerodynamics) #Aircraft exhaust emissions #Jet nozzles #Plumes (Fluid dynamics) |
| Tipo |
text |
