Silton et al., 2014 - Google Patents
Effect of Projectile Aft End on Stability, Range, and ManeuverabilitySilton et al., 2014
- Document ID
- 561744351338740173
- Author
- Silton S
- Fresconi F
- Publication year
- Publication venue
- 32nd AIAA Applied Aerodynamics Conference
External Links
Snippet
RECISION munition research is currently an area of focus throughout the United States armed services. Within the US Army, rolling projectiles using movable lifting surfaces for maneuver control have been and are continuing to be developed. 1, 2. However, the …
- 230000000694 effects 0 title description 21
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Silton et al. | Effect of canard interactions on aerodynamic performance of a fin-stabilized projectile | |
Schütte | Numerical investigations of vortical flow on swept wings with round leading edges | |
Bhagwandin | High-alpha prediction of roll damping and magnus stability coefficients for finned projectiles | |
Bhagwandin | Numerical prediction of roll damping and Magnus dynamic derivatives for finned projectiles at angle of attack | |
Silton | Navier-Stokes predictions of aerodynamic coefficients and dynamic derivatives of a 0.50-cal projectile | |
Bhagwandin et al. | Numerical prediction of pitch damping derivatives for a finned projectile at angles of attack | |
DeSpirito et al. | CFD prediction of M910 projectile aerodynamics: unsteady wake effect on magnus moment | |
Nguyen et al. | Investigations on missile configuration aerodynamic characteristics for design optimization | |
Owens | Weissinger's model of the nonlinear lifting-line method for aircraft design | |
Sahu et al. | Aeromechanics and control of projectile roll using coupled simulation techniques | |
DeSpirito et al. | Computational fluid dynamics analysis of a missile with grid fins | |
Pasiliao et al. | Preliminary aero-thermal structural simulation | |
El-Mahdy et al. | A comparative study of prediction techniques for supersonic missile aerodynamic coefficients | |
Silton et al. | Effect of Projectile Aft End on Stability, Range, and Maneuverability | |
Paul et al. | Influence of bending locations and angles on the aerodynamic performance of a bent body projectile | |
Silton et al. | Effect of Canard Deflection on Fin Performance of a Fin-Stabilized Projectile | |
DeSpirito | CFD validation of interaction of fin trailing vortex with downstream control surface in high subsonic flow | |
Silton et al. | Comparison of uncoupled and coupled CFD-based simulation techniques for the prediction of the aerodynamic behavior of a complex projectile | |
Weinacht et al. | Computation of the roll characteristics of a finned projectile | |
Venkatachari et al. | Transition analysis for the CRM-NLF wind tunnel configuration using transport equation models and linear stability correlations | |
Akgül et al. | Numerical investigation of NASA tandem control missile and experimental comparison | |
Roy et al. | Estimation of numerical error for 3D inviscid flows on Cartesian grids | |
Doraiswamy et al. | Detached eddy simulations and Reynolds-averaged Navier-Stokes calculations of a spinning projectile | |
NIETUBICZ | Navier-Stokes computations for conventional and hollow projectile shapes at transonic velocities | |
Coyle et al. | CFD aerodynamic characterization of a high maneuverability airframe |