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Experimental investigation and analysis of two sources of nozzle-thrust misalignment
- Publication Year :
- 1970
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1970.
-
Abstract
- Asymmetry of nozzle's throat produces oscillatory type net side-force axial profile. Using mean values of localized static pressure and Mach number, scaling laws for flat-plate supersonic flow over protrusion are applied to nozzle expansion cone irregularities to give approximate indication of perturbed-pressure profiles and induced side forces.
- Subjects :
- Mechanics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19700000392
- Document Type :
- Report