Aerodynamic analysis of complex missile configurations using AVUS (Air Vehicles Unstructured Solver)

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2004, Pages 1307-1345

  Hoke, Captain Charles ^a   Burnley, Victor ^a   Schwabacher, Captain Gregory ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CATAPULTS (AIRCRAFT LAUNCHERS); COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; FINS (HEAT EXCHANGE); METHOD OF MOMENTS; MILITARY OPERATIONS; SUPERSONIC FLOW; VORTEX FLOW; WINGS;

AERODYNAMIC ANALYSIS; AIR VEHICLE UNSTRUCTURED SOLVER (AVUS); COMPLEX MISSILE CONFIGURATION; SURFACE PRESSURE;

AERODYNAMICS;

EID: 20544457718     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5452     Document Type: Conference Paper

References (6)

1. 60: A Parallel Implicit, Unstructured Euler/Navier-Stokes Flow Solver," AIAA Paper 99-0786, January 1999.
2. Pirzadeh, S., "Three-Dimensional Unstructured Viscous Grids by the Advancing-Layers Method," AIAA Journal, Vol. 34, No. 1, January 1996, pp. 43-49.
3. Godunov, S.K., "A Finite Difference Method for the Numerical Calculation of Discontinuous Solutions of Equations of Fluid Dynamics," Sbornik Mathematics, Vol. 47, pp. 271-290, 1959.
4. Menter, F. R., "Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows," AIAA Paper 93-2906, July 1993.
5. Allen, Jerry. "KTA Square Body Missile, Unitary Plan Wind Tunnel Test 1757," Internal report, NASA Langley Research Center Configuration Aerodynamics Branch
6. Graves, Ernald B. "Aerodynamic Characteristics of a Monoplane Missile Concept With Bodies of Circular and Elliptical Cross Section," NASA Technical Memorandum 74079, December 1977