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The purpose of this handbook is to provide customers of the Lockheed Martin Missiles and Fire Control (LMMFC) High Speed Wind Tunnel (HSWT) and related services with information necessary for planning and scheduling model design or testing. Our HSWT facility can accommodate a wide variety of high-speed tests including aerodynamic force measurements, flutter, store drop trajectories, inlet performance evaluation, jet engine base-flow simulation and dynamic stability. Detailed descriptions of the wind tunnel circuit capabilities, data acquisition and processing capabilities, model support system, special test systems and techniques, and model design considerations are provided in this handbook. Information for planning and scheduling testing is also included. High speed wind tunnel facility overview : Facility Description 2.1.1 Occupancy Charge Policy 2.1.2 Security 2.2 Additional Facilities and Services 2.3 Wind Tunnel Operating Capabilities. WIND TUNNEL CIRCUIT CAPABILITIES : Compression and Storage 3.2 Flow Control 3.3 Variable Contour Nozzle 3.4 Test Sections and Diffusers 3.4.1 Supersonic Test Section 3.4.2 Transonic Test Section 3.5 Performance and Operational Characteristics 3.5.1 Performance Parameters 3.5.2 Calibration Data 3.5.3 Operational Characteristics. DATA ACQUISITION AND PROCESSING CAPABILITIES 4.1 Data Acquisition and Processing System 4.2 Dynamic Data Recording Equipment 4.3 Steady-State Force Instrumentation 4.4 Steady-State Pressure Instrumentation 4.5 Data Processing and Reporting. MODEL DESIGN CONSIDERATIONS 7.1 General Design Considerations 7.2 Model Size 7.3 Model Placement 7.4 Pressure and Internal Flow Models 7.5 Static Stability Force Model Design Considerations 7.6 Starting Loads and Factors of Safety. TEST PLANNING AND SCHEDULING 8.1 Test Scheduling 8.2 Model Delivery Information. Illustration : High Speed Wind Tunnel General Arrangement, High Speed Wind Tunnel Circuit Layout, Model Setup Room and Calibration Stand, Model Setup Room Machine Shop Tools for Model Repairs and Modifications. Typical Model and Roll Mechanism Assembly.
Tags : lockheed martin missiles, wind tunnel facility, general design considerations, test systems design, variable contour, information illustration, pressure instrumentation, force measurements, calibration data, model placement, flow simulation, lockheed martin, performance parameters, factors of safety, aerodynamic force
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