Bibliografías temáticas / Hawker aircraft

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Literatura académica sobre el tema "Hawker aircraft"

Autor: Grafiati
Publicado: 26 de julio de 2024
Última modificación: 31 de julio de 2025

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Artículos de revistas sobre el tema "Hawker aircraft"

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Anton, N., and R. M. Botez. "Weight functions method for stability analysis applied as design tool for Hawker 800XP aircraft." Aeronautical Journal 119, no. 1218 (2015): 981–98. http://dx.doi.org/10.1017/s0001924000004280.

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Abstract A new method for system stability analysis, the weight functions method, is applied to estimate the longitudinal and lateral stability of a Hawker 800XP aircraft. This paper assesses the application of the weight functions method to a real aircraft and a method validation with an eigenvalues stability analysis of the linear small-perturbation equations. The method consists of finding the weight functions that are equal to the number of differential equations required for system modelling. The aircraft’s stability is determined from the sign of the total weight function – the sign shou
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Anton, N., R. M. Botez, and D. Popescu. "New methodology and code for Hawker 800XP aircraft stability derivatives calculation from geometrical data." Aeronautical Journal 114, no. 1156 (2010): 367–76. http://dx.doi.org/10.1017/s0001924000003821.

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Abstract The new FDerivatives code was conceived and developed for calculating static and dynamic stability derivatives of an aircraft in the subsonic regime, based on its geometrical data. The code is robust and it uses geometries and flight conditions to calculate the aircraft’s stability derivatives. FDerivatives contains new algorithms and methods that have been added to DATCOM’s classical method, presented in a USAF Stability and Control DATCOM reference. The new code was written using MATLAB and has a complex structure which contains a graphical interface to facilitate the work of potent
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Taranu, Liviu. "THE VFW 614 FOKKER PROJECT AND THE ROMANIAN AERONAUTICAL INDUSTRY IN THE 1970s." Review of the Air Force Academy 19, no. 2 (2021): 49–53. http://dx.doi.org/10.19062/1842-9238.2021.19.2.7.

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n a ‘70s meeting of the Socialist Republic of Romania’s (RSR) Defense Council, Nicolae Ceausescu decided to have Romanians build a short-courier aircraft capable of ensuring passenger traffic, domestic and foreign, over short distances. Based on these indications, a contact was designed and several offers were obtained for the joint construction of such an aircraft: the British company "BAC" for an aircraft to be designed and developed at the request of the Romanian side, the British company "Hawker Siddeley, for the HS 748 aircraft, already manufactured in a military version, subject to obtai
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Sunny, Okemini Uguzo, Nwevo Obinnaya, Chinemerem Gideon Japheth, Johnson Anamemena Nnaemeka, and Yekini Bello. "DESIGNED AND ANALYSIS OF AN SC-17M MAIN LANDING GEAR LOADING ACTION." FUTA JOURNAL OF ENGINEERING AND ENGINEERING TECHNOLOGY 16, no. 1 (2022): 20–26. http://dx.doi.org/10.51459/futajeet.2022.16.1.339.

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The concept of SC-17M aircraft design was initiated to address the shortfalls on the DO-228 and Hawker Beechcraft King Air 350i aircraft. Until recently by using a standard specification, an SC-17M landing gear design has been carried out. Detailed study of sub-part C of the certification standard aided the application and determination of the necessary loads on the landing gear. The comprehensive design employed 300M steel as the best structural material to be used in the fabrication of the landing gear. The maximum bending moment in the shock absorber and wheel axle were calculated and valid
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Bore, C. L. "Some contributions to propulsion theory — Fuel consumption formulae and general range equation." Aeronautical Journal 97, no. 963 (1993): 118–20. http://dx.doi.org/10.1017/s0001924000025203.

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The permanent urgency of aircraft design during the author’s career at Hawker Aircraft, a.k.a. British Aerospace Kingston, inhibited publication of his advances of theory. So he collected those on propulsion and presented them to the Royal Aeronautical Society in a lecture “Some Unpublished Contributions to Propulsion Theory” on 11 March 1992. The meeting proposed that the material should be published in full, and F. W. Armstrong helpfully suggested that the best way for future reference would be to divide the material into Technical Notes on related topics, each capable of standing alone. The
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GRIGORAS, Georgiana, Ioana VIZIREANU, Bogdan URITESCU, and Andreea CALCAN. "Avalanche risk analysis using airborne LiDAR data." INCAS BULLETIN 14, no. 1 (2022): 25–38. http://dx.doi.org/10.13111/2066-8201.2022.14.1.3.

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Natural and man-made disasters are a justified concern causing life-threats damages, affects existing budgets or disrupts national economic and social development plans. In this paper, a digital terrain model (DTM) and a geographic information system (GIS) are used to identify areas with a high risk of avalanches in the Râmeț mountain area of Alba County. Avalanches are the result of a complex interaction between terrain, weather conditions and snow cover characteristics. The most important factor among those listed is the terrain, being the only constant parameter over time. Therefore, the pr
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Williams, J. E. D. "Air Navigation Systems Chapter I. Astronomical Navigation in the Air 1919–1969." Journal of Navigation 42, no. 1 (1989): 73–91. http://dx.doi.org/10.1017/s0373463300015101.

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As the marine sextant is only useful to low-flying aircraft because of its reliance on the sea horizon (see Section 1), many earlier pioneers descended almost to sea level to take their sights; but as Alcock and Brown were the first to discover, it is often necessary to climb above the cloud in order to see the sky. Some pioneers used the horizon of stratocumulus cloud below, among them K. M. Grieve who, with Hawker, would have been the first across the Atlantic if radiator trouble had not made them the first survivors of a mid-Atlantic aeroplane ditching. As Grieve was so happy with his cloud
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Ko, Samuel Y., and George M. Rice. "Multiple E-2D Hawkeye Aircrew with Neurocognitive Symptoms During a Single Over-Pressurization Episode." Aerospace Medicine and Human Performance 91, no. 12 (2020): 970–74. http://dx.doi.org/10.3357/amhp.5682.2020.

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BACKGROUND: Increased frequencies of physiological episodes have been a significant concern for Naval Aviation for the last several years. These include several aircraft platforms, but no previously documented E-2D Hawkeye events. This report documents an episode in an E-2D, with multiple aircrew affected at the same time.CASE REPORT: While deployed aboard a U.S. aircraft carrier, five E-2D Hawkeyes aircrew were simultaneously exposed to the same over-pressurization during a routine sortie. Out of the five aircrew, four immediately reported hypoxic-like neurocognitive symptoms of mental slowin
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Baggaley, W. J., V. Porubčan, R. L. Hawkes, et al. "Commission 22: Meteors and Interplanetary Dust: (Meteores Et Poussiere Interplanetaire)." Transactions of the International Astronomical Union 24, no. 1 (2000): 156–69. http://dx.doi.org/10.1017/s0251107x00002819.

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The IAU Meteor Data Centre (MDC), maintained at Lund, Sweden, under the direction of Bertil Lindblad, remains a valuable resource for the meteor community. Commission 22 currently has representatives on two inter-commission Working Groups, The Prevention of Interplanetary Pollution (Chair C. S. L. Keay of Commission 22) and Near-Earth Objects (IAU C22 representative I.P. Williams). The Commission has one Working Group of its own, Amateur-Professional Co-operation in Meteors, consisting of P. Jenniskens (Chair), H. Betlem, N. Bone, P. Brown, T. Cooper, I. Hasegawa, R. Hawkes, G. Klar-Renner, V.
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Sippel, Jason A., Scott A. Braun, Fuqing Zhang, and Yonghui Weng. "Ensemble Kalman Filter Assimilation of Simulated HIWRAP Doppler Velocity Data in a Hurricane." Monthly Weather Review 141, no. 8 (2013): 2683–704. http://dx.doi.org/10.1175/mwr-d-12-00157.1.

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Abstract This study utilizes ensemble Kalman filter (EnKF) observing system simulation experiments (OSSEs) to analyze the potential impact of assimilating radial velocity observations of hurricanes from the High-altitude Imaging Wind and Rain Airborne Profiler (HIWRAP). HIWRAP is a new Doppler radar mounted on the NASA Global Hawk unmanned airborne system that flies at roughly 19-km altitude and has the benefit of a 25–30-h flight duration, which is 2–3 times that of conventional aircraft. This research is intended as a proof-of-concept study for future assimilation of real HIWRAP data. The mo
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Tesis sobre el tema "Hawker aircraft"

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Alexander, Kristy, Mike Bender, Rick Boisvert, and Mike Gibson. "Cost Benefit Analysis of Options to Manage E-2C Hawkeye Aircraft Techincal Data." Thesis, Monterey, California. Naval Postgraduate School, 2011. http://hdl.handle.net/10945/7067.

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EMBA Project Report<br>EXECUTIVE SUMMARY: Program Management Aircraft Office 231 (PMA231) is tasked with providing “cradle to grave” acquisition support to the U.S. Navy’s fleet of E-2C Hawkeye airborne early warning aircraft. A major portion of this support centers on providing and updating integrated logistics support (ILS) elements, which include technical data. Effective and efficient management of aircraft technical data ensures that the Navy’s aviation maintenance personnel have the most accurate, up to date technical manuals available. Availability of these manuals forms a critical lin
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Williams, Robert K. "Developmental flight test of a powered approach stability augmentation system on the U.S. Navy's E-2C Hawkeye 2000 aircraft." 2002. http://etd.utk.edu/2002/WilliamsRobert.pdf.

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Thesis (M.S.)--University of Tennessee, Knoxville, 2002.<br>Title from title page screen (viewed Feb. 28, 2003). Thesis advisor: Ralph Kimberlin. Document formatted into pages (x, 59 p. : ill.). Vita. Includes bibliographical references (p. 46-47).
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Ohman, Klas Walace. "How they flew modern flight test of pioneering Wright aircraft /." 2004. http://etd.utk.edu/2004/OhmanKlas.pdf.

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Thesis (M.S.)--University of Tennessee, Knoxville, 2004.<br>Title from title page screen (viewed Sept. 27, 2004). Thesis advisor: R.B. Richards. Document formatted into pages (xi, 83 p. : ill. (some col.)). Vita. Includes bibliographical references (p. 63-65).
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Libros sobre el tema "Hawker aircraft"

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Mason, Francis K. Hawker aircraft since 1920. 3rd ed. Naval Institute Press, 1991.

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Mason, Francis K. Hawker aircraft since 1920. 3rd ed. Putnam Aeronautical, 1991.

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M, Clarke R., ed. Hawker Hurricane Portfolio: A Brooklands Aircraft Portfolio. Brooklands Books, 1986.

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Clarke, R. M. Hawker Typhoon Portfolio: A Brooklands Aircraft Portfolio. Brooklands Books, 1987.

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Robert, Jackson. Hawker Hunter: The operational record. Smithsonian Institution Press, 1990.

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Robert, Jackson. Hawker Hunter: The operational record. Airlife Publ.Ltd., 1989.

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Transportation Safety Board of Canada. Calm Air Ltd., Hawker Siddeley HS-748 C-GEPB, Brochet, Manitoba, 30 April 1991. Transportation Safety Board of Canada, 1994.

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Transportation Safety Board of Canada. Runway excursion, Calm Air International Ltd., Hawker Siddeley HS 748-2A C-GD0P, Thompson, Manitoba, 20 January 1994. Transportation Safety Board of Canada, 1994.

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9

United States. National Transportation Safety Board. Aircraft accident report: Air Illinois Hawker Siddley HS 748-2A, N748LL, near Pinckneyville, Illinois, October 11, 1983. The Board, 1985.

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10

Barnes, F. G. British Aerospace 748: Including Avro, Hawker Siddeley, Hindustan Aeronautics built aircraft and H.S. 780 Andover C.Mk. 1. Air-Britain (Historians) Ltd, 1986.

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Capítulos de libros sobre el tema "Hawker aircraft"

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"No. 28569. Agreement between the Government of Australia and the Government of New Zealand concerning Royal New Zealand Air Force Sky hawk Aircraft involvement in Australian defence force air defence support flying. Signed at Canberra on 13 July 1990." In United Nations Treaty Series. UN, 2000. http://dx.doi.org/10.18356/14724047-en-fr.

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Actas de conferencias sobre el tema "Hawker aircraft"

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Zhao, Jinggen. "Full-Aircraft UH-60M Loads and Performance Correlations at Level and Maneuvering Flight Conditions with HELIOS-RCAS." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-254.

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The Sikorsky BLACK HAWK® is the primary medium lift helicopter for the U.S. Army performing a wide range of missions that encompass Air Assault, MEDEVAC, CSAR, Command and Control, and VIP transport. The Multimission UH-60M is one of the latest in the BLACK HAWK helicopter product family, more capable, more survivable, more maintainable, more powerful, and more effective than its predecessors. In previous efforts, a high-fidelity CFDCSD based full-aircraft trim and maneuvering simulation methodology was developed and applied to model both coaxial aircraft and single main/tail rotor configurati
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McGinty, Robert, Steven Lamb, Gregory Wood, and Jeff Brenna. "Determination of Flight Loads for the HH-60G Pave Hawk Helicopter." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10254.

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This paper presents the testing and analysis methods used in determination of HH-60G flight loads using data gathered during a series of flight strain surveys. Analysis methods and results are emphasized here as most testing methods and data have been shared in previous forums. This is followed by a discussion of the resulting computed load values and their verification through comparisons to operational parameters such as aircraft weight, engine torque, and G-loads. It is found that computed loads and moments compare very well to flight conditions. For example, main rotor lift force correlate
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Brookhart, Andrew, Chris Lyman, Mark Davis, et al. "Flight Test Preparation of Health Management Technologies." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11474.

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The U.S. Army traditionally has used a time-based, on-condition maintenance paradigm that relies on at-aircraft inspections and periodic in-depth phase inspections to determine condition and ensure airworthiness. The result is a significant maintenance burden, both scheduled and unscheduled, and excessive aircraft downtime. The objective of the Aviation Development Directorate (ADD) and Sikorsky Aircraft Corporation (SAC) Capability-Based Operations and Sustainment Technology-Aviation (COST-A) program was to develop and demonstrate an integrated set of high value diagnostics, prognostics, and
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Vayalali, Praneet, Michael McKay, Jayanth Krishnamurthi, and Farhan Gandhi. "Swashplate Actuator Failure Compensation for UH-60 Black Hawk in Cruise using Horizontal Stabilator." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0074-2018-12789.

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A flight simulation model for the UH-60 Black Hawk based on Sikorsky's GenHel model is modified to simulate a locked failure of a main rotor swashplate servo actuator and is compensated by using the stabilator as a redundant control effector. Steady state trim analysis is performed to demonstrate feasibility of trimmed flight in various conditions with different locked servo actuator positions for the forward, aft, and lateral actuators. A model-following, linear dynamic inversion controller is implemented and modified to account for locked actuator position. Post-failure, the control mixing a
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Finckenor, Jeff. "A SUMS Based Usage Spectrum for the UH-60M ITE Equipped Black Hawk." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1119.

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Previous work documented the use of IVHMS data on the U.S. Army's fleet of UH-60 Black Hawk helicopters to update the fatigue lives of six specific components on the A/L and M models. This paper documents a significant expansion of the level of data applied to the usage spectrum, as well as applying it to all components on the aircraft. As a design spectrum for the yet to be fielded Improved Turbine Engine (ITE) equipped UH-60M, changes due to new engine capability needed to be addressed. The new spectrum has been developed and is being used for planning of flight testing. The spectrum along w
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Carter, Casey, Tim Willis, Travis Grant, Scott Rosengren, Matthew Lawrence, and Todd Stanley. "A Modular Open System Approach for the H-60M Black Hawk &ndash; Following the Future Vertical Lift Framework." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-404.

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The H-60 Black Hawk remains a cornerstone of U.S. Army Aviation, but its legacy avionics architecture presents modernization challenges. To ensure long-term operational relevance and interoperability with future platforms like the Future Long Range Assault Aircraft (FLRAA), the Army is implementing a Modular Open Systems Approach (MOSA). This strategy facilitates rapid technology integration, enhances sustainment efficiency, and mitigates obsolescence. The Army's MOSA adoption aligns with regulatory mandates such as the National Defense Authorization Act and Department of Defense (DoD) acquisi
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Brookhart, Andrew, Chris Lyman, Mark Davis, et al. "Flight Testing of Health Management Technologies." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12080.

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The U.S. Army traditionally has used a time-based, on-condition maintenance paradigm that relies on at-aircraft inspections and periodic in-depth phased inspections to determine condition and ensure airworthiness. The result is a significant maintenance burden, both scheduled and unscheduled, and excessive aircraft downtime. The objective of the Aviation Development Directorate (ADD) and Sikorsky Aircraft Corporation (SAC) Capability-Based Operations and Sustainment Technology-Aviation (COST-A) program was to develop and demonstrate an integrated set of high value diagnostics, prognostics, and
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8

Cheung, Catherine, Bruno Rocha, Julio Valdés, and Jobin Puthuparampil. "Improved Load Estimation And Fatigue Life Tracking Demonstrated On Multiple Platforms Using The Signal Approximation Method." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11475.

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This paper presents the results from several load estimation methods developed at the National Research Council Canada (NRC) which enable the estimation of helicopter loads and tracking load exceedances and fatigue damage for a targeted component using computational intelligence techniques. The approach relies only on flight state and control system (FSCS) parameters, such as those recorded by a flight data recorder (FDR), and can also be applied to legacy aircraft or to those aircraft not equipped with HUMS. The methodologies adapt to the input data available so are not constrained to one par
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Schrage, Daniel, and Alex Van. "A DAVBA Approach for Complex VTOL Aircraft Development." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10269.

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As aircraft systems become more complex the need to integrate software and hardware at different levels of abstraction becomes more important. For complex civil aircraft USA and Europe have reached a consensus in "Guidelines for Development of Civil Aircraft and Systems Development" in SAE ARP 4754A/ED-79. This document discusses the development of aircraft systems taking into account the overall aircraft operating environment and functions. This includes validation of requirements and verification of the design implementation for certification and product assurance. It provides practices for
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Bates, Preston, Treven Baker, Mark Davis, et al. "Capability-Based Operations and Sustainment – Aviation (COST-A) Technology Development." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10193.

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The U.S. Army traditionally has used a time-based, on-condition maintenance paradigm that relies on at-aircraft inspections and periodic in-depth phase inspections to determine condition and ensure airworthiness. The result is a significant maintenance burden, both scheduled and unscheduled, and excessive aircraft downtime. The objective of the Aviation Development Directorate-Aviation Applied Technology Directorate (ADD-AATD) and Sikorsky Aircraft Corporation (SAC) Capability-Based Operations and Sustainment Technology-Aviation (COST-A) project was to develop and demonstrate an integrated set
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Informes sobre el tema "Hawker aircraft"

1

Lemmon, John. E-2D Advanced Hawkeye Aircraft (E-2D AHE). Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada613398.

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Lemmon, John. E-2D Advanced Hawkeye Aircraft (E-2D AHE). Defense Technical Information Center, 2015. http://dx.doi.org/10.21236/ad1019142.

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Wright, Nathan L. Assessment of Cargo Space Seating Performance Applicable to Pave Hawk and Black Hawk Aircraft During Helicopter Mishaps. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada565472.

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