Applied computational aerodynamics

Book · Sun Dec 31 23:00:00 EST 1989

OSTI ID:6080168

Henne, P A

The present volume discusses the original development of the panel method, the mapping solutions and singularity distributions of linear potential schemes, the capabilities of full-potential, Euler, and Navier-Stokes schemes, the use of the grid-generation methodology in applied aerodynamics, subsonic airfoil design, inverse airfoil design for transonic applications, the divergent trailing-edge airfoil innovation in CFD, Euler and potential computational results for selected aerodynamic configurations, and the application of CFD to wing high-lift systems. Also discussed are high-lift wing modifications for an advanced-capability EA-6B aircraft, Navier-Stokes methods for internal and integrated propulsion system flow predictions, the use of zonal techniques for analysis of rotor-stator interaction, CFD applications to complex configurations, CFD applications in component aerodynamic design of the V-22, Navier-Stokes computations of a complete F-16, CFD at supersonic/hypersonic speeds, and future CFD developments.

• OSTI ID: 6080168
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
330600 -- Advanced Propulsion Systems-- Vehicle Design Factors
42 ENGINEERING
420400* -- Engineering-- Heat Transfer & Fluid Flow
99 GENERAL AND MISCELLANEOUS
990200 -- Mathematics & Computers
ABSTRACTS
AERODYNAMICS
AIRCRAFT
AIRFOILS
CALCULATION METHODS
COMPUTERIZED SIMULATION
DESIGN
DIFFERENTIAL EQUATIONS
DOCUMENT TYPES
DRAG
EQUATIONS
EQUATIONS OF MOTION
FLUID FLOW
FLUID MECHANICS
LEADING ABSTRACT
MECHANICS
MESH GENERATION
NAVIER-STOKES EQUATIONS
PARTIAL DIFFERENTIAL EQUATIONS
PROPULSION SYSTEMS
SIMULATION
SUBSONIC FLOW
TRANSITION FLOW
TRANSONIC FLOW