Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests
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| Published in | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES Vol. 65; no. 3; pp. 134 - 137 |
|---|---|
| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Tokyo
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
01.01.2022
Japan Science and Technology Agency |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0549-3811 2189-4205 |
| DOI | 10.2322/tjsass.65.134 |
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| ArticleNumber | T-21-18 |
|---|---|
| Author | UENO, Makoto YAMADA, Kento UCHIYAMA, Takahiro |
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| References | 2) Hoerner, S. F.: Fluid-dynamic Drag, Private Publishing, 1965, pp. 2-1–2-16. 4) Webb, L. D., Whitmore, S. A., and Janssen, R. L.: Preliminary Flight and Wind Tunnel Comparisons of the Inlet/Airframe Interaction of the F-15 Airplane, AIAA Paper 79-0102, 1979. 9) Kohzai, M., Ueno, M., Shiohara, T., and Sudani, N.: Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel, AIAA Paper 2008-848, 2008. 5) Tomita, H. and Naruoka, M.: JAXA Flying Test Bed “Hisho,” Aeronautical and Space Sciences Japan, 62, 6 (2014), pp. 195–201 (in Japanese). 8) Braslow, A. L. and Knox, E. C.: Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers from 0 to 5, NACA TN 4363, 1958. 6) Yasue, K., Ueno, M., Naruoka, M., and Nakakita, K.: Flight Test for Static Aerodynamic Characteristics of the JAXA Flying Test Bed “Hisho,” 53rd Aircraft Symposium, Matsuyama, Ehime, Japan, JSASS-2015-5182, 2015 (in Japanese). 3) Raymer, D. P.: Aircraft Design: a Conceptual Approach, 5th ed., American Institute of Aeronautics and Astronautics, Reston, 2012, pp. 429–438. 12) Re, R. J.: An Investigation of Several NACA 1-Series Axisymmetric Inlets at Mach Numbers from 0.4 to 1.29, NASA TM, X-2917, 1974. 7) Saijo, M., Yasue, K., Ueno, M., Naruoka, M., and Nakakita, K.: Systematic Uncertainty Analysis of Aerodynamic Coefficients Obtained by Flight Tests Using the JAXA Flying Test Bed “Hisho,” J. Jpn. Soc. Aeronaut. Space Sci., 65, 3 (2017), pp. 135–136 (in Japanese). 10) Paterson, J. H., MacWilkinson, D. G., and Blackerby, W. T.: A Survey of Drag Prediction Techniques Applicable to Subsonic and Transonic Aircraft Design, AGARD Aerodynamic Drag, Neuilly-sur-Seine, France, CP-124, 1973. 11) Heidebrecht, A., Stankowski, T., and MacMaus, D.: Parametric Geometry and CFD Process for Turbofan Nacelles, ASME Turbo Expo 2016 Turbomachinery Technical Conference and Exposition, Seoul, South Korea, GT2016-57784, 2016. 1) Kimzey, W. F., Covert, E. E., Rooney, E. C., Richey, G. K., and James, C. R.: Thrust and Drag: Its Prediction and Verification, American Institute of Aeronautics and Astronautics, Reston, 1985, pp. 173–206. 11 1 12 2 3 4 5 6 7 8 9 10 |
| References_xml | – reference: 6) Yasue, K., Ueno, M., Naruoka, M., and Nakakita, K.: Flight Test for Static Aerodynamic Characteristics of the JAXA Flying Test Bed “Hisho,” 53rd Aircraft Symposium, Matsuyama, Ehime, Japan, JSASS-2015-5182, 2015 (in Japanese). – reference: 7) Saijo, M., Yasue, K., Ueno, M., Naruoka, M., and Nakakita, K.: Systematic Uncertainty Analysis of Aerodynamic Coefficients Obtained by Flight Tests Using the JAXA Flying Test Bed “Hisho,” J. Jpn. Soc. Aeronaut. Space Sci., 65, 3 (2017), pp. 135–136 (in Japanese). – reference: 3) Raymer, D. P.: Aircraft Design: a Conceptual Approach, 5th ed., American Institute of Aeronautics and Astronautics, Reston, 2012, pp. 429–438. – reference: 8) Braslow, A. L. and Knox, E. C.: Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers from 0 to 5, NACA TN 4363, 1958. – reference: 2) Hoerner, S. F.: Fluid-dynamic Drag, Private Publishing, 1965, pp. 2-1–2-16. – reference: 10) Paterson, J. H., MacWilkinson, D. G., and Blackerby, W. T.: A Survey of Drag Prediction Techniques Applicable to Subsonic and Transonic Aircraft Design, AGARD Aerodynamic Drag, Neuilly-sur-Seine, France, CP-124, 1973. – reference: 11) Heidebrecht, A., Stankowski, T., and MacMaus, D.: Parametric Geometry and CFD Process for Turbofan Nacelles, ASME Turbo Expo 2016 Turbomachinery Technical Conference and Exposition, Seoul, South Korea, GT2016-57784, 2016. – reference: 4) Webb, L. D., Whitmore, S. A., and Janssen, R. L.: Preliminary Flight and Wind Tunnel Comparisons of the Inlet/Airframe Interaction of the F-15 Airplane, AIAA Paper 79-0102, 1979. – reference: 1) Kimzey, W. F., Covert, E. E., Rooney, E. C., Richey, G. K., and James, C. R.: Thrust and Drag: Its Prediction and Verification, American Institute of Aeronautics and Astronautics, Reston, 1985, pp. 173–206. – reference: 9) Kohzai, M., Ueno, M., Shiohara, T., and Sudani, N.: Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel, AIAA Paper 2008-848, 2008. – reference: 5) Tomita, H. and Naruoka, M.: JAXA Flying Test Bed “Hisho,” Aeronautical and Space Sciences Japan, 62, 6 (2014), pp. 195–201 (in Japanese). – reference: 12) Re, R. J.: An Investigation of Several NACA 1-Series Axisymmetric Inlets at Mach Numbers from 0.4 to 1.29, NASA TM, X-2917, 1974. – ident: 2 – ident: 1 doi: 10.2514/4.865732 – ident: 3 – ident: 5 – ident: 7 doi: 10.2322/jjsass.65.135 – ident: 12 – ident: 9 doi: 10.2514/6.2008-848 – ident: 11 – ident: 6 – ident: 8 – ident: 4 doi: 10.2514/6.1979-102 – ident: 10 |
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| SubjectTerms | Capture Area Ratio Flight Reynolds Number Aerodynamics Flight Testing Spillage Drag Wind Tunnel Testing Wind tunnels |
| Title | Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests |
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