The nozzle is for use with a rocket or other jet type motor. Cams are employed to shift the nozzle venturi axially with respect to a fixed conical probe projecting through it to thereby change the size of the unobstructed area of the throat orifice.
Variable Throat Nozzle
1965
1 pages
Report
No indication
English
NTIS | 1965
|Design of variable-throat rectangular nozzle for supersonic wind tunnel
Engineering Index Backfile | 1947
|Annular throat rocket nozzle design
TIBKAT | 1961
|Computational Characterization of a CD Nozzle with Variable Geometry Translating Throat
Springer Verlag | 2018
|Nozzle Aerodynamic Stability During a Throat Shift
NTRS | 2005
|