Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage
Tilt-rotor aircraft has both vertical take-off and high-speed cruise capability, and has been widely applied in many fields. It is of great significance to study the take-off performance design of the tilt-rotor aircraft in the short take-off mode. A series of approaches have been developed to ident...
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2018-08-01
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| Series: | Hangkong gongcheng jinzhan |
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| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018004?st=article_issue |
| _version_ | 1811326256322445312 |
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| author | Qi Wantao |
| author_facet | Qi Wantao |
| author_sort | Qi Wantao |
| collection | DOAJ |
| description | Tilt-rotor aircraft has both vertical take-off and high-speed cruise capability, and has been widely applied in many fields. It is of great significance to study the take-off performance design of the tilt-rotor aircraft in the short take-off mode. A series of approaches have been developed to identify the short take-off performance of tilt-rotor aircraft which tilt their nacelles to implement short take-off. The approaches include how to identify the minimum tilt angle of the nacelle, and the formulas suitable to calculate lift-off speed and take-off length are also developed. These methods are adopted in the design of a certain tilt-rotor aircraft during the preliminary design stage, moreover, the effects of airport altitude and weather conditions on short take-off performance are also researched. The results are reasonable, which indicate that these approaches are useful and of great value in practice. |
| first_indexed | 2024-04-13T14:46:56Z |
| format | Article |
| id | doaj.art-619502c13575485ebf2c39e0deb7115f |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-04-13T14:46:56Z |
| publishDate | 2018-08-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-619502c13575485ebf2c39e0deb7115f2022-12-22T02:42:43ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902018-08-019336336710.16615/j.cnki.1674-8190.2018.03.0092018-06-28Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design StageQi Wantao0The General Configuration and Aerodynamics Design and Research Department, The First Aircraft Institute, Xi'an 710089, ChinaTilt-rotor aircraft has both vertical take-off and high-speed cruise capability, and has been widely applied in many fields. It is of great significance to study the take-off performance design of the tilt-rotor aircraft in the short take-off mode. A series of approaches have been developed to identify the short take-off performance of tilt-rotor aircraft which tilt their nacelles to implement short take-off. The approaches include how to identify the minimum tilt angle of the nacelle, and the formulas suitable to calculate lift-off speed and take-off length are also developed. These methods are adopted in the design of a certain tilt-rotor aircraft during the preliminary design stage, moreover, the effects of airport altitude and weather conditions on short take-off performance are also researched. The results are reasonable, which indicate that these approaches are useful and of great value in practice.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018004?st=article_issuetilt-rotor aircraftshort take-offperformance |
| spellingShingle | Qi Wantao Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage Hangkong gongcheng jinzhan tilt-rotor aircraft short take-off performance |
| title | Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage |
| title_full | Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage |
| title_fullStr | Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage |
| title_full_unstemmed | Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage |
| title_short | Research on Design Method of Short Take-off Performance of Tilt-rotor Aircraft during Preliminary Design Stage |
| title_sort | research on design method of short take off performance of tilt rotor aircraft during preliminary design stage |
| topic | tilt-rotor aircraft short take-off performance |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018004?st=article_issue |
| work_keys_str_mv | AT qiwantao researchondesignmethodofshorttakeoffperformanceoftiltrotoraircraftduringpreliminarydesignstage |