面向机舰适配的舰载飞机起降特性分析

doi:10.7527/S1000-6893.2015.0309

Abstract

Abstract:

Carrier suitability is a particular integral of carrier-based aircraft design including two items,aircraft performance compatibility and shipborne supportability.Its essential refers to the inherent capabilities of carrier-based aircraft to utilize fully and efficiently the characteristics,facilities and equipment of the carrier.Starting from the analyses of carrier-based aircraft operational environments,the items for a good carrier suitability is first defined at home in this paper.After that,based on the situations of making the land-based aircraft compatible with ski-jump and arresting devices,focusing on the flight performance the process of recovery and launch is physically described,which is identified as two phases:flat deck run and cured deck run,and the quantitated effects of wind over deck on the take-off and landing based on the data from foreign aircraft carrier.Meanwhile,from the viewpoint of safe recovery,landing pattern,standardized recovery procedure and the minimum length for aircraft bolter are all proposed.A last section is devoted to the relevant items concerning ski-jump and catapult launch aircraft served for aircraft carrier.

Key words: carrier suitability, ski-jump, arresting landing, wind over deck, carrier-based aircraft, aircraft carrier

CLC Number:

V119

WANG Yongqing, LUO Yunbao, WANG Qitao, ZHANG Yong. Carrier suitability-oriented launch and recovery characteristics of piloted carrier-based aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(1): 269-277.

References

[1] KNOTT R C.The naval aviation guide[M].3rd ed.Maeryland:Naval Institute Press Annapolis,1985.
[2] LAWRENCE J T.Milestones and developments in US naval carrier aviation-part Ⅱ:AIAA-2005-6120[R].Reston:AIAA,2005.
[3] BRIMSKI F O.Aircraft design for carrier operations[C]//Society of Allied Weight Engineers 55th Annual International Conference.Los Angeles,California:Society of Allied Weight Engineers,Inc.,1996:1-43.
[4] Naval Air Engineering Center.Technical data requirements for shipboard and shore based vertical/short takeoff and landing:NAEC-AWS-571[S].New Jersey:NAEC,1974.
[5] Naval Air Warfare Center Aircraft Division.Carrier suitability test manual:SA FTM-01[S].Maryland:Flight Test and Engineering Group(SA70A),1994.
[6] LOFTUS J,PIEKARSKI B.Carrier suitability tests of the Rafale airplane in the United States:AIAA-1994-2173[R].Reston:AIAA,1994.
[7] DECKER R M.Carrier suitability test[C]//Adversory Groupfor Aerospace Research & Development.Nuilly Sur Seine,France:North Atlantic Treaty Organization,1977:1-16.
[8] ANON.Aircraft carrier data reference manual[M].2nd ed.New Jersey:NAEC,1995.
[9] KITOWSKI J V.Fighter airframe/propulsion integration-A general dynamics perspective:AIAA-1992-3332[R].Reston:AIAA,1992.
[10] BENJAMIN G O.Future jet technologies.Part A[J].International Journal of Turbo & Jet-engines,2011,28:1-20.
[11] MARECA RIOS R,MONTES BARRENETXEA J,ESQUISABEL ALEGRIA X,et al.Efficient flight control by use of EJ200 thrust vectoring[J].Journal of Aerospace Science & Technologies,2009,61(1):219-231.
[12] FOZARD J W.Ski-jump-A geeat jump for tactical airpower:AIAA-1979-0696[R].Reston:AIAA,1979.
[13] FUREY R J.Short distanced performance using a gravity assist ski jump:ADA124456[R].Virjinia,USA:DTIC,1983.
[14] FRY A,COOK R,REVILL N.CVF ski-jump ramp profile optimization for F-35B[J].The Aeronautic Journal,2009,113(1140):79-85.
[15] HULL D G.Fundamentals of airplane flight mechanics[M].Berlin:Springer Verlag,2007:16-23.
[16] SHINAR J,EHRENTAL D,REUVENI R.Optimization of ski-jump performance:AIAA-1985-45946[R].Reston:AIAA,1985.
[17] PATERSIONIRCRAFT G A.Creteria for determination of minimium usable approach speed:AIAA-1967-0578[R].Reston:AIAA,1967.
[18] OLSEN J J.Optimization performance parameters for ski-jump operations of USAF fighter aircraft:ADA148532[R].Virjinia,USA:DTIC,1984.
[19] DOUGHERTY L,ROLSTON D R.Simulator evaluation of F/A-18 ski jump:AIAA-1985-40553[R].Reston:AIAA,1985.
[20] NELSON J H,GRIFFIN G M.United States Navy pilot-controlled landing procedure and associated equipment[C]//Adversory Group for Aerospace Research & Development.Nuilly Sur Seine,France:North Atlantic Treaty Organization,1963.
[21] Commander Naval Air Systems Command.Carrier air traffic control handbook:NAVAIR AE-CVATC-OPM-000[S].Mryland,USA:Naval Air Test Center,1994.
[22] Naval Air Systems Command.NAVAIR 00-80T-105 CV NATOPS manual[S].California,USA:Naval air system command,2009.
[23] Department of Defense.Catapulting and arresting gear forcing functions for aircraft structural design:MIL-HDBK-2066(AS)[S].Washington,D.C.:Department of Defense,1989.
[24] WALKER G,WURTH S,FULLER J D R.F-35B integrated flight-propulsion control development:AIAA-2013-4243[R].Reston:AIAA,2013.

Carrier suitability-oriented launch and recovery characteristics of piloted carrier-based aircraft

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	FU Jiawei, YU Jialong, LIU Chao, WANG Muguo, WANG Zizi. Key technologies of aerodynamics design of stealth carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525804-525804.
[2]	WANG Xiao, CHENG Jianhui, SHEN Tianrong, XU Baocheng, MENG Xuan. Numerical simulation research of influence of wake flow field on inlet temperature field of carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525795-525795.
[3]	CHEN Yueliang, CHEN Liang, BIAN Guixue, YANG Xiangning, GUAN Yu, ZHANG Yong, HE Gang. Corrosion protection control and calendar life design of advanced carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525786-525786.
[4]	LIU Dong, WU Jiaren, ZHOU Yizhou, LIU Zhenxiang, LI Yu, WANG Mingze. Practice and prospects of comprehensive support technologies of carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525802-525802.
[5]	WANG Yongqing. Fixed-wing carrier-based aircraft: Key technologies and future development [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525859-525859.
[6]	WANG Yongqing, YU Hao, SHI Yan. Dynamics and kinematics characteristics of carrier-based aircraft ski-jump take-off [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525853-525853.
[7]	CAO Qikai, WANG Yan, YAO Niankui, HE Gang, CHEN Zhongming, ZHANG Guijiang, TIAN Zhiliang, WU Xinyue. Development and application of strength design technology of advanced carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525793-525793.
[8]	JIANG Qideng. Statistical modeling and prediction of arresting force for carrier-based aircraft based on flight parameters [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 224030-224030.
[9]	LIU Jie, HAN Wei, XU Weiguo, LIU Chun, YUAN Peilong, CHEN Zhigang, PENG Haijun. Optimal path tracking control of carrier-based aircraft on the deck based on RHC [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(8): 322842-322842.
[10]	YANG Xuan, WEI Xiaoyong, CUI Delong. Bus interface strategy in flight control system for carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622283-622283.
[11]	MA Kaichao, XU Lanling, ZHANG Jianye. Flight load design of aileron of carrier-based transport category aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622262-622262.
[12]	DUAN Zhuoyi, WANG Wei, GENG Jianzhong, HE Daquan, MA Kun. Precision trajectory manual control technologies for carrier-based aircraft approaching and landing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622328-622328.
[13]	ZUO Xianshuai, WANG Lixin, LIU Hailiang, WANG Yun, ZHANG Yu. Similarity for simulating automatic carrier landing process of full-scale aircraft with scaled-model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 123005-123005.
[14]	QU Yepin, JIN Huiming, HE Zhaoxiong. Carrier-based aircraft equipment system-of-systems and index demonstration method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(5): 221675-221675.
[15]	HE Min, ZHU Xiaolong, LIU Xiaoming, LIU Fan, YAO Xiaohu. Impact response of ground ejection of front fuselage structure of carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(5): 221711-221711.