ディスク・ローディング
出典: フリー百科事典『ウィキペディア（Wikipedia）』 (2022/09/19 04:35 UTC 版)
実例
| 機種 | 区分 | 最大全備重量 | 総ディスク面積 | 最大ディスク・ローディング |
|---|---|---|---|---|
| ロビンソン R22 | 汎用軽ヘリコプター | 1,370 lb (635 kg) | 497 ft² (46.2 m²) | 2.6 lb/ft² (14 kg/m²) |
| ベル 206B3 | 汎用ターボシャフトヘリコプター | 3,200 lb (1,451 kg) | 872 ft² (81.1 m²) | 3.7 lb/ft² (18 kg/m²) |
| CH-47D チヌーク | タンデムローターヘリコプター | 50,000 lb (22,680 kg) | 5,655 ft² (526 m²) | 8.8 lb/ft² (43 kg/m²) |
| ミル Mi-26 | 大型輸送ヘリコプター | 123,500 lb (56,000 kg) | 8,495 ft² (789 m²) | 14.5 lb/ft² (71 kg/m²) |
| CH-53E | 大型輸送ヘリコプター | 73,500 lb (33,300 kg) | 4,900 ft² (460 m²) | 15 lb/ft² (72 kg/m²) |
| MV-22B オスプレイ | ティルトローター V/STOL機 | 60,500 lb (27,400 kg) | 2,268 ft² (211.4 m²) | 26.68 lb/ft² (129.63 kg/m²) |
- ^ Keys, C. N.; Stepniewski, W. Z. (1984). Rotary-wing aerodynamics. New York: Dover Publications. pp. 3. ISBN 0-486-64647-5. "It is interesting to note that there has always been a strong intuitive association of rotary-wing aircraft with low disc loading which is reflected in the commonly accepted name of rotor given to their lifting airscrews."
- ^ Wang, James M.; Jones, Christopher T.; Nixon, Mark W. (1999-05-27). “A Variable Diameter Short Haul Civil Tiltrotor”. 55th Annual Forum of the American Helicopter Society. Montreal, Canada. "The variable diameter tiltrotor (VDTR) is a Sikorsky concept aimed at improving tiltrotor hover and cruise performance currently limited by disk loading that is much higher in hover than conventional helicopter, and much lower in cruise than turbo-prop systems."
- ^ Rotorcraft Flying Handbook. U.S. Government Printing Office, Washington D.C.: U.S. Federal Aviation Administration. (2000). pp. 2–4, 19-3, G-2. FAA-8083-21. "DISC LOADING—The total helicopter weight divided by the rotor disc area."
- ^ Maisel, Martin D., Demo J. Giulianetti and Daniel C. Dugan. NASA SP-2000-4517, "The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight" (PDF) p2. NASA, 2000. Accessed: 17 March 2012.
- ^ Noor, Ahmed Khairy (1996). Future Aeronautical and Space Systems (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Astronautics). pp. 66. ISBN 1-56347-188-4. "Reduced disk loading in the vertical mode also results in lower downwash and improved capability for autorotation."
- ^ Leishman, J. Gordon. "Development of the Autogiro : A Technical Perspective Archived 2005-12-31 at the Wayback Machine." page 5. Hofstra University, New York, 2003.
- ^ Birdsall, David (1996). Aircraft Performance. Cambridge: Cambridge University Press. pp. 99. ISBN 0-521-56836-6. "contra-rotating propellers this rotational loss can be eliminated and maximum efficiencies approaching 0.9 can be obtained even with high disc loading"
- ^ Reinhard Hilbig; Wagner, Siegfried; Ulrich Rist; Hans-Joachim Heinemann (2002). New Results in Numerical and Experimental Fluid Mechanics III. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. 3. Berlin: Springer. p. 82. ISBN 3-540-42696-5. "The A400M will be driven by four modern turboprop engines with a high disc loading.... The disc loading of the propellers is significantly higher than realised on former tactical transport aircraft like C130H or Transall C160."
- ^ Johnson, Wayne (1994). “2”. Helicopter theory. New York: Dover Publications. pp. 28–34. ISBN 0-486-68230-7. "In the momentum theory analysis the rotor is modeled as an actuator disk, which is a circular surface of zero thickness that can support a pressure difference and thus accelerate the air through the disk."
- ^ Principles of Helicopter Aerodynamics (Cambridge Aerospace Series). Cambridge, UK: Cambridge University Press. (2006). ISBN 0-521-85860-7
「ディスク・ローディング」の続きの解説一覧
- ディスク・ローディングのページへのリンク
