Aerodynamic Force Analysis. Volume I
Aerodynamic Force Analysis. Volume I
- Neue Suche nach: B. D. Djordjevic
- Neue Suche nach: B. D. Djordjevic
Aerodynamic Force Analysis methods and technology from an extensive bibliography, originally prepared as an internal reference for the U. S. Army Missile Command, is presented in conjunction with definitive guidance for use and applicability. An altitude range from 0 to 400,000 feet and a Mach number range from low subsonic through oribital-re-entry level hypersonic is encompassed, with appropriate continuum, slip and free molecule flow treatments.
Dokumentinformationen
Aerodynamic Force Analysis. Volume I
1966
520 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Aerodynamics , Fluid mechanics , Force(Mechanics) , Fluid dynamics , Hypersonic flow , Subsonic flow , Transonic flow , Supersonic flow , Numerical methods and procedures , Numerical analysis , Angle of attack , Sideslip , Aerodynamic loading , Heat transfer , Rarefied gas dynamics , Partial differential equations , Geometric forms , Configuration , Hydrodynamics , Aerodynamic characteristics , Reynolds number , Knudsen number , Fluid flow , Altitude , Velocity , Continuum mechanics , Pressure , Drag , Temperature , Density , Skin friction , Tables(Data) , Experimental data
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