Predicting Wing Drop in the Harrier II Using the Static Wind Tunnel Test and Analysis Technique CBSTAT-Reference-Cited by-同舟云学术

Predicting Wing Drop in the Harrier II Using the Static Wind Tunnel Test and Analysis Technique CBSTAT

Published:2004-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
language:
Short-container-title:

Author:

Payne Philip¹,McConnell Jeff²

Affiliation:

1. BAE SYSTEMS (North America)

2. Lockheed Martin Aeronautics Co.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5050

Reference28 articles.

1. Continuous Beta Sweep Test & Analysis Technique (CBSTAT) for Predicting Wing Drop Based on Static Wind Tunnel Testing

2. Wind Tunnel Investigation of Pre-Production F/A-18E Lateral Characteristics Using Continuous Beta Sweep Test & Analysis Technique (CBSTAT)

3. 75 0.8 0.85 0.9 0.75 0.5 < Mach 0.75 0.8 0.85 0.9 0.75 0.5 < Mach Alpha Beta Alpha Beta Ap 0 239 187 219,273 132 310 276 273,274 repeats a3 -6 215 An 240 188 220,274 133 311 277 a5 -1.2 335 From = 0 Ap -2.5 241 189 221 134 306 278 a5 -1.2 336 From = -5 An 242 190 222 135 307 279 a5 -1 266 Ap 2.5 243 191 223 136 308 280 a6 0 216 An 244 192 224 137 309 281 a7 -2 268 a1 Bp,Bn 246,247 193,194 225,226 172,173 a7 2 269 a2 248,249 195,196 227,228 174,175 313,314 282,283 a8 -8 267 a3 250,251 197,198 229,230 176,177 315,316 a8 -2 270 From = 0 a4 217,218 a9 -2 271 From = -5 a5 252,253 199,200 231,232 178,179 317,318 a9 2 186 a6 254,255 201,202 233,234 180,181 319,320 284,285 a9 4 214 a7 256,257 203,204 235,236 182,183 321,322 286,287 a10 1.2 304 a8 258,259 205,206 237,238 184,185 323,324 288,289 a10 4.5 337 a9 260,261 207,208 325,326 290,291 a14 -5 305 a10 262,263 209,210 327,328 292,293 a11 264,265 211,212 329,330 294,295 a12 331,332 296,297 a13 333,334 298,299 a14 300,301 a15 302,303

4. Table 2 CBSTAT HUD Severity Grading Installed in the ARA Transonic Wind Tunnel

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