Fuselage Aerodynamic Prediction Methods-Reference-Cited by-同舟云学术

Fuselage Aerodynamic Prediction Methods

Published:2015-06-19 Issue: Volume: Page:
ISSN:
Container-title:33rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Nicolosi Fabrizio¹,Della Vecchia Pierluigi¹,Ciliberti Danilo¹,Cusati Vincenzo¹,Attanasio Lorenzo¹

Affiliation:

1. University of Naples "Federico II"

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2257

Reference33 articles.

1. 45 9.35 75.5 2.58 -0.3088 -0.3021 -0.3150 -2.0% -2% -0.0511 -0.0489 -0.0521 Test 1 3.45 9.35 75.5 2.58 -0.2714 -0.2811 -0.3126 3.4% -15% -0.0449 -0.0465 -0.0518 Test 2 3.45 9.35 75.5 2.58 -0.2484 -0.2421 -0.3169 -2.6% -28% -0.0411 -0.0401 -0.0525 Test 3 3.45 9.35 75.5 2.58 -0.3023 -0.3045 -0.3102 0.7% -3% -0.0501 -0.0504 -0.0514 Test 4 (ATR72)

2. 63 6.03 61 2.37 -0.2310 -0.2180 -0.2711 -6.0% 25% -0.0382 -0.0361 -0.0288

3. Test 5 3.15 7.79 75.5 2.58 -0.3493 -0.3632 -0.3156 4.0% 10% -0.0578 -0.0601 -0.0523

4. 45 9.35 75.5 2.58 0.1756 0.1789 0.2012 2.0% -15% 0.0291 0.0296 0.0333 Test 1 3.45 9.35 75.5 2.58 0.1639 0.1638 0.1884 -0.1% -15% 0.0271 0.0271 0.0312 Test 2 3.45 9.35 75.5 2.58 0.2358 0.2333 0.2412 -1.1% -2% 0.0390 0.0386 0.0399 Test 3 3.45 9.35 75.5 2.58 0.1547 0.1504 0.1786 -2.8% -15% 0.0256 0.0249 0.0296 Test 4 (ATR72)

5. 63 6.03 61 2.37 0.2519 0.2243 0.1931 -11.0% 23% 0.0249 0.0222 0.0191

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