Relevant bibliographies by topics / Longitudinal static stability

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Longitudinal static stability'

Author: Grafiati
Published: 4 June 2021
Last updated: 15 February 2022

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Journal articles on the topic "Longitudinal static stability"

1

WANG, KeMu, ChenAn ZHANG, FaMin WANG, and ZiAn JIA. "Longitudinal static stability analysis of hypersonic waveriders." SCIENTIA SINICA Technologica 44, no. 10 (October 1, 2014): 1114–22. http://dx.doi.org/10.1360/n092014-00058.

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Bloy, A. W. "An Aircraft Longitudinal Static Stability and Control Experiment." International Journal of Mechanical Engineering Education 24, no. 3 (July 1996): 183–90. http://dx.doi.org/10.1177/030641909602400305.

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3

ANDO, Shigenori, and Hiroshi KAJITA. "Evaluation Method of Longitudinal Static Stability of Tailless Airplane." Journal of the Japan Society for Aeronautical and Space Sciences 40, no. 456 (1992): 14–22. http://dx.doi.org/10.2322/jjsass1969.40.14.

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Su, Xin Bing, Zhou Zhou, Jing Cheng Shi, and Xu Wang. "Research on Longitudinal Static Stability for VFSW Tailless Configuration UAV." Applied Mechanics and Materials 543-547 (March 2014): 348–53. http://dx.doi.org/10.4028/www.scientific.net/amm.543-547.348.

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The Variable Forward-Swept Wing (VFSW) Tailless configuration UAV can well satisfy multipurpose demands. However, this kind of unconventional morphing aircraft lacks tail, which brings great challenge to stability analysis. The connatural aero-elasticity divergence and the strong aerodynamic coupling as well as many uncertain factors in mechanical environment, give the VFSW Tailless configuration UAV complicated dynamic characteristics. During the process of transformation, the variation of dynamic shape will inevitably lead to the variation about aerodynamic center and barycentre positions of airplane, then make the angle of attack static stability margin variable, and directly influence stability of aircraft. On the basis of introduction of the VFSW Tailless configuration UAV, according to its geometric shape, positions of aerodynamic center and barycentre, in different states with different forward-swept angle, were calculated, so as to obtain variation curve of longitudinal static stability margin, which provided preferences for dynamics analysis, position of barycentre adjustment and design of flight control system (FCS).
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Choi, Jung-Kyu, and Hyoung-Tae Kim. "Evaluation of Longitudinal Static Stability of Human Powered Hydrofoil Boat." Journal of the Society of Naval Architects of Korea 46, no. 4 (August 20, 2009): 391–97. http://dx.doi.org/10.3744/snak.2009.46.4.391.

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Yang, Wei, Zhigang Yang, and Maurizio Collu. "Longitudinal static stability requirements for wing in ground effect vehicle." International Journal of Naval Architecture and Ocean Engineering 7, no. 2 (March 2015): 259–69. http://dx.doi.org/10.1515/ijnaoe-2015-0018.

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7

Bai, Ming, He Xu, Long He, Wei Xing Guo, and Chang Hua Qiu. "Longitudinal Associated Stability Analysis of Mobile Robot in Rough Terrain." Key Engineering Materials 572 (September 2013): 632–35. http://dx.doi.org/10.4028/www.scientific.net/kem.572.632.

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Focusing on the longitudinal adaptability of a three-fuselage articulated with separated differential mechanism in rough terrain, the associated factor which could be a criterion for the judgment of longitudinal associated stability of mobile robot has been proposed, and the analysis results of the longitudinal associated stability under different situation have been obtained based on static stability theory of mobile robot.
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Cook, M. V. "The theory of the longitudinal static stability of the hang-glider." Aeronautical Journal 98, no. 978 (October 1994): 292–304. http://dx.doi.org/10.1017/s0001924000026798.

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Abstract This paper describes the development of a simple theory of the longitudinal static stability of the hang-glider. The classical theory, as developed for the conventional aeroplane, is modified to accommodate the particular features of the hang-glider. When the appropriate assumptions are made, the theory provides simple insight into the controls fixed and controls free stability and control characteristics of the hang-glider. The validity of the theoretical models is successfully demonstrated by application to a typical fifth generation hang-glider wing for which good quality aerodynamic data were available.
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Yang, Wei, Zhigang Yang, and Chengjiong Ying. "Effects of design parameters on longitudinal static stability for WIG craft." International Journal of Aerodynamics 1, no. 1 (2010): 97. http://dx.doi.org/10.1504/ijad.2010.031705.

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Xiao, Hou Di, Pan Pan Mi, Long Bin Liu, and Shuai Cao. "A New Method of Strengthening Longitudinal Static Stability of Airship in Ascent." Applied Mechanics and Materials 687-691 (November 2014): 212–15. http://dx.doi.org/10.4028/www.scientific.net/amm.687-691.212.

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To improve the controllability and maneuverability, airship is usually designed as static instability. But the airship is vulnerable to sudden wind interference in its ascent, resulting in divergent pitching motion. A new aerodynamic shape was put forward which added a inflatable aerodynamic-lift wing at backward of the airship hull. With the method of Computational Fluid Dynamics (CFD), aerodynamic characteristics and longitudinal static stability of the conventional airship and new winged airship were comparative investigated. It can be concluded that the new winged airship was longitudinal stable whereas the conventional airship was instable. It can be applied for restraining the sudden wind interference for airship in ascent.
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Dissertations / Theses on the topic "Longitudinal static stability"

1

Kilkenny, E. A. "An experimental study of the longitudinal aerodynamic and static stability characteristics of hang gliders." Thesis, Cranfield University, 1986. http://dspace.lib.cranfield.ac.uk/handle/1826/11096.

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A mobile experimental test facility has been developed to carry out the aerodynamic evaluation of hang glider wings normally performed in a wind tunnel. Longitudinal aerodynamic data obtained using this facility is presented for three modern hang glider wings, a Silhouette, Demon 175 and Magic 166, together with surface flow patterns for the latter two wings. The longitudinal stability criterion are studied and alternatives established, equivalent to the stick fixed and stick free criterion for conventional aircraft, relevant to weight shift controlled wings. These are based on the pilot's position and control force to trim. The aerodynamic data obtained from the mobile facility is used to calculate these parameters and the longitudinal static stability of each wing is examined. The influence of several rigging parameters, variable by the pilot before flight, on the longitudinal static stability and control of the hang glider are also investigated.
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Kóňa, Marián. "Aerodynamický návrh transsonického bezpilotního kluzáku." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232008.

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This master thesis is focused on aerodynamic design of transonic glider, which is assigned for following an airliner at cruising regime of flight. Main goal of the thesis is to determine basic geometrical design of airplane with respect to Whitcomb aera rule, mass analysis and drag polar. Weight analysis includes determining center of gravity according to longitudinal static stability margin. The drag polar of the airplane is determine for cruising regime of flight, that means the regime of following an airliner.
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"Longitudinal Static Stability of a Tethered Rotorcraft." Master's thesis, 2017. http://hdl.handle.net/2286/R.I.43975.

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abstract: This thesis discusses the equilibrium conditions and static stability of a rotorcraft kite with a single main tether flying in steady wind conditions. A dynamic model with five degrees of freedom is derived using Lagrangian formulation, which explicitly avoids any constraint force in the equations of motion. The longitudinal static stability of the steady flight under constant wind conditions is analyzed analytically from the equilibrium conditions. The rotorcraft kite orientation and tether angle are correlated through the equation Γ=δ-ϑ, a necessary condition for equilibrium. A rotorcraft kite design with 3kg mass and 1.25m rotor radius is found to be longitudinally statically stable at 25,000ft with Γ>〖65〗^0 for wind speeds above 19m/s.
Dissertation/Thesis
Masters Thesis Aerospace Engineering 2017
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4

Jamison, Glenn Richard. "Flight test investigation of propeller effects on the static longitudinal stability of the E-2C airplane." 2006. http://etd.utk.edu/2006/JamisonGlenn.pdf.

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Books on the topic "Longitudinal static stability"

1

Hinds, H. A. Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk. Cranfield, Bedford: College of Aeronautics, Cranfield Institute of Technology, 1990.

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2

Brandon, Jay M. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. Hampton, Va: Langley Research Center, 1986.

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3

Center, Langley Research, ed. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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4

Center, Langley Research, ed. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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Book chapters on the topic "Longitudinal static stability"

1

Keller, Dennis. "Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a Transport Aircraft with Circulation Control." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 13–22. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-03158-3_2.

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2

"Static Longitudinal Stability Theory." In Flight Testing Of Fixed-Wing Aircraft, 209–21. Reston ,VA: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/5.9781600861840.0209.0221.

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3

"Trim and Longitudinal Static Stability." In Performance of the Jet Transport Airplane: Analysis Methods, Flight Operations and Regulations, 613–25. Chichester, UK: John Wiley & Sons, Ltd, 2017. http://dx.doi.org/10.1002/9781118534786.app5.

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4

"Static Longitudinal Stability Flight Test Methods." In Flight Testing Of Fixed-Wing Aircraft, 223–33. Reston ,VA: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/5.9781600861840.0223.0233.

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5

"Design methods for bodies with invariable longitudinal static stability factor." In Series on Advances in Mathematics for Applied Sciences, 95–128. WORLD SCIENTIFIC, 1995. http://dx.doi.org/10.1142/9789812797223_0003.

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6

Paula Ribeiro, Ana. "Biomechanical Aspects of the Static and Dynamic Patterns of the Feet of Runners with Plantar Fasciitis and Their Relationship with Sports Shoes." In Recent Advances in Sport Science [Working Title]. IntechOpen, 2021. http://dx.doi.org/10.5772/intechopen.97090.

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The purpose of this literature review was to evaluate studies that have investigated static and dynamic biomechanical patterns of the feet in runners with plantar fasciitis, as well as their relationship with sports shoes and insoles prescription. Original articles with different design on this theme were considered. In general, the increase plantar load rates in runners with plantar fasciitis may be directly related to changes in the plantar arch (elevated) and the rearfoot alignment in pronation, as well as the effect of shoes or insoles to reduce heel pain. In summary, the clinical support of the literature review was showed that a decrease in the medial longitudinal arch induces greater mobility of the foot, which promotes a greater angle of rearfoot pronation to maintain the stability of the subtalar joint during static and dynamic feet support in activities, such as running. This results in a greater overload on the medial region of the calcaneus, producing greater stress on the plantar fascia, contributing to the development and progression of plantar fasciitis in runners. In addition, treatment of acute plantar fasciitis was associate to insoles while chronic phase associated for shoes ultra-flexible intermediate midsole for heel pain reduction and improvement foot biomechanics in runners with plantar fasciitis.
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Conference papers on the topic "Longitudinal static stability"

1

Anwar-ul-Haque, Waqar Asrar, Ashraf A. Omar, Erwin Suleiman, and Jaffar M. Ali. "Static longitudinal stability of a hybrid airship." In 2014 11th International Bhurban Conference on Applied Sciences and Technology (IBCAST). IEEE, 2014. http://dx.doi.org/10.1109/ibcast.2014.6778167.

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2

Claar, P. W., and J. Yan. "Skid-Steer Loader Performance and Static Longitudinal Stability Analysis." In 1988 SAE International Off-Highway and Powerplant Congress and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1988. http://dx.doi.org/10.4271/881311.

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Liu, Chaoqiang. "An Estimation Method for Aircraft Longitudinal Static Stability Prior to Flight Test." In 2nd International Conference on Computer Application and System Modeling. Paris, France: Atlantis Press, 2012. http://dx.doi.org/10.2991/iccasm.2012.352.

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4

Westin, Michelle Fernandino, and Ricardo Luiz Utsch de Freitas Pinto. "A Wing-by-Wing Approach for Biplane Static Longitudinal Stability and Control Analysis." In 2008 SAE Brasil Congress and Exhibit. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2008. http://dx.doi.org/10.4271/2008-36-0247.

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Matějů, Jiří. "Simple universal nonlinear longitudinal flight simulation with avoiding of static and dynamic stability derivatives." In 13th Research and Education in Aircraft Design. Brno: Fakulta strojniho inzenyrstvi VUT v Brne, 2019. http://dx.doi.org/10.13164/conf.read.2018.13.

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Coelho, Thiago Campos Gondim Martins, and Ricardo Luiz Utsch de Freitas Pinto. "Development of equations for longitudinal static stability and control calculus adapted to all-flying tail." In 2006 SAE Brasil Congress and Exhibit. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2006. http://dx.doi.org/10.4271/2006-01-2788.

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7

FRAZIER, WAYNE. "Longitudinal and directional static stability effects of a large radome mounted atop a 747-200 aircraft." In Aircraft Design and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3173.

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8

OSTOWARI, C., and D. NAIK. "An experimental study of the lift, drag and static longitudinal stability for a three lifting surface configuration." In 24th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-398.

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9

Boling, Jeremy S., and Gecheng Zha. "Numerical Investigation of Longitudinal Static Stability of a High-Speed Tandem-Wing VTOL Vehicle Using CoFlow Jet Airfoil." In AIAA Scitech 2021 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-1732.

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10

Liang, Zhen, and Weijun Wang. "Estimation of the Effect of Lift-drag Ratio caused by Relaxing Longitudinal Static Stability of a certain-type of Joined-Wing Aircraft." In 2018 International Conference on Mechanical, Electronic, Control and Automation Engineering (MECAE 2018). Paris, France: Atlantis Press, 2018. http://dx.doi.org/10.2991/mecae-18.2018.118.

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Reports on the topic "Longitudinal static stability"

1

AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA. Volume II. Flying Qualities Phase. Chapter 5: Longitudinal Static Stability. Fort Belvoir, VA: Defense Technical Information Center, October 1990. http://dx.doi.org/10.21236/ada319976.

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