Applied computational aerodynamics

Book · Mon Jan 01 00:00:00 EST 1990

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
• Resource Relation: Related Information: Progress in Astronautics and Aeronautics. Volume 125
• Country of Publication: United States
• Language: English

Related Subjects

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