Tactical missile aerodynamics : prediction methodology
著者
書誌事項
Tactical missile aerodynamics : prediction methodology
（Progress in astronautics and aeronautics, v. 142）
American Institute of Aeronautics and Astronautics, c1992
2nd ed
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注記
The first edition of Tactical Missile Aerodynamics ... was Volume 104 of the Progress in Astronautics and Aeronautics series (AIAA, New York, 1986) -- pref.
内容説明・目次
内容説明
Prediction Methodology contains updated versions of nine chapters from the first edition and chapters on drag prediction, component build-up methods, Euler methods and Navier-Stokes solvers. Special attention is paid to nonlinear flow phenomena and unconventional airframe shapes. Eight colour plates and more than 540 figures are included.
目次
- Tactical Missile Drag
- Drag Prediction Methods for Axisymmetric Missile Bodies
- Introduction to the Aerodynamic Heating Analysis of Supersonic Missiles
- The Component Build-Up Method for Engineering Analysis of Missiles at Low-to-High Angles of Attack
- Analysis Methods and Experiments for Missiles with Noncircular Fuselages
- Vortex Cloud Model for Body Vortex Shedding and Tracking
- Panelling Methods with Vorticity Effects and Corrections for Nonlinear Compressibility
- Supersonic Full-Potential Methods for Missile Body Analysis
- Space Marching Euler Solvers
- Time-Asymptotic Euler/Navier-Stokes Methods for Subsonic/Transonic Flows
- Three-Dimensional Boundary Layers on Missiles
- Navier-Stokes Analyses of Flows over Slender Airframes
- Exhaust Plumes and Their Interaction with Missile Airframes - a New Viewpoint.
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