Roll-yaw control at high angle of attack by forebody tangential blowing /
| Data(s) |
31/12/1969
|
|---|---|
| Resumo |
"October 1995." Cover title. Mode of access: Internet. |
| Formato |
bib |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
[Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University, |
| 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 | #Angle of attack (Aerodynamics) #Yawing (Aerodynamics) #Flight control. |
| Tipo |
text |
