Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 15

No. 26205 Overexpanded nozzle No. 26206 Isentropic expansion No. 26207 Underexpanded nozzle No. 26213 Uniform and perturbed flow No. 26214 Physical space airfoil No. 26215 Compressibility corrections and experimental results No. 26220 Critical Mach number estimation No. 26221 Airfoil thickness and critical Mach number effect No. 26222 NACA 0012 airfoil No. 26223 Low-speed pressure coefficient over NACA 0012 airfoil surface No. 26224 Critical Mach number No. 26225 NACA 0012 pressure coefficient, 0.575 freestream Mach No. 26226 NACA 0012 pressure coefficient, 0.725 freestream Mach No. 26227 Drag coefficient vs Mach number No. 26228 Large drag rise beside Mach 1 No. 26229 Streamwise thickness-to-chord ratio vs Mach number No. 26232 Non-area-ruled aircraft schematic No. 26233 Non-area-ruled aircraft cross section No. 26234 Non-area-ruled aircraft area distribution No. 26235 Area-ruled aircraft planview No. 26236 Area-ruled aircraft area distribution No. 26237 Drag coefficient vs freestream Mach number No. 26238 NACA 64-series properties at cruise lift conditions No. 26239 Pressure coefficient for NACA 64-series airfoil No. 26240 Supercritical airfoil No. 26241 Pressure coefficient for supercritical airfoil No. 26242 Drag divergence for NACA 64-series and supercritical airfoil No. 26243 Mach number contours for NACA 0012 airfoil in transonic flow No. 26244 Initial wing design No. 26245 Pressure coefficient on initial wing design No. 26246 Optimized wing design No. 26247 Pressure coefficient on optimized wing design No. 26248 Pressure coefficient at 44.3% of span No. 26249 Pressure coefficient at 27.2% of span No. 26250 Pressure coefficient at 9.6% of span No. 26251 Legend for optimized transonic wing No. 26252 Optimized transonic wing with upper-surface isobars No. 26253 Pressure coefficient at 95.6% of span No. 26254 Pressure coefficient at 79.1% of span No. 26255 Pressure coefficient at 60.8% of span No. 26256 Linearized supersonic flow No. 26257 Supersonic and subsonic linearized pressure coefficiant No. 26258 Linearized supersonic flow No. 26260 F-16 transonic area ruling No. 26261 F-16 supersonic area ruling No. 26262 Actual vs purposed F-16 supersonic area ruling No. 26281 Shock layers for hypersonic flow No. 26282 Shock layers for hypersonic flow: detail No. 26283 Non-viscous interaction flat plate pressure graph No. 26284 Viscous interaction flat plate pressure graph
 

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