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Design Features of Supercritical Aerofoil
• Blunt nose-
rapid p pressure reduction around leading edge
• Flat top-
Reduce the flow acceleration on upper surface toreduce shock strength
• Cusped trailing edge-
Increased loading over rear of aerofoil to recoversome lift
Velocity vector
Speed of NACA
Thin-skinned Structures The SCB geometry can't be used because the skins are too flexible. Instead, a centre-notch flexure (CNF) test can be used. A hole is drilled abo
Depreciation Methods Technically speaking, U.S. tax law permits deduction from taxable income of a reasonable allowance for wear or tear, natural decay or decline, exhaustion,
Static electricity in aircraft: As mentioned earlier, the effects of static electricity are of considerable importance in the design of aircraft and aircraft equipment. An air
Active clearance control system The system provides fan discharge air for cooling the core compartment and the low-pressure turbine case. At low altitudes the core engine requ
Alternative escape routes: Does everyone have access to the alternative routes or do some people have no choice about which way they go? Are all the escape routes
VDD=20V,RG=1MOHM,RD=3.3KOHM,RS=1KOHM,IDSS=8MA,VP=-6V
explain data model with example?
Composites have low shear strengths compared to longitudinal strengths. The ILSS test is a simple 3 point bend test, requiring a small amount of material. A span to depth ratio
Hi
Ewing’s molecular theory of magnetism Every molecule of a magnetic substance behaves as a tiny magnet called molecular magnet. In an unmagnetized state the molecular m
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