Relevant bibliographies by topics / Flight 712

Contents

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

Academic literature on the topic 'Flight 712'

Author: Grafiati
Published: 4 June 2021
Last updated: 28 July 2025

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Journal articles on the topic "Flight 712"

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Wang, Lin Lin, and Ge Gao. "Stability Features of the Saucer-Shaped Blend-Wing-Body Aircraft." Advanced Materials Research 712-715 (June 2013): 1307–11. http://dx.doi.org/10.4028/www.scientific.net/amr.712-715.1307.

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The saucer-shaped aircraft is a novel aircraft adopting blend-wing-body configuration. The linear perturbation theory based on the classic flight dynamics was used to analyze the longitudinal, lateral and directional flight qualities of the saucer-shaped aircraft under low speed conditions. The flight qualities were given. Meanwhile the aerodynamic characteristics of the saucer-shaped aircraft, the conventional aircraft and the flying wing aircraft were also contrasted to discuss their similarities and differences. The results show that the saucer-shaped aircraft has stable longitudinal mode,
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YOSHIDA, Hiroshi, Jun NAKAYA, Naoki MAEDA, et al. "712 A Reusable Hybrid Rocket System : Its Nominal Design and Flight Capability Predictions." Proceedings of Conference of Hokkaido Branch 2001.41 (2001): 252–53. http://dx.doi.org/10.1299/jsmehokkaido.2001.41.252.

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Ramírez-Molina, César, Olivier Heudi, Mark Pullen, and Peter S. Marshall. "Study of bradykinin metabolism by rat lung tissue membranes and rat kidney brush border membranes by HPLC with inductively coupled plasma—mass spectrometry and orthogonal acceleration time-of-flight mass spectrometry." Journal of Peptide Science 12, no. 3 (2006): 220–26. http://dx.doi.org/10.1002/psc.712.

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Zeng, Yao Yuan, Wen Tao Zhao, and Zheng Hua Wang. "Hybrid MPI + OpenMP Parallelization of Scramjet Simulation with Hypergraph Partitioning." Advanced Materials Research 712-715 (June 2013): 1294–97. http://dx.doi.org/10.4028/www.scientific.net/amr.712-715.1294.

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As one of the most significant methods to study hypersonic flight vehicle, the numerical simulation of supersonic combustion ramjet has drawn an ever increasing attention at present. Nevertheless, the traditional serial simulation cannot satisfy the practical needs because of high calculation precision, avaricious memory overhead and overlong computation time. In this paper, we study on a general algorithm for scramjet simulation, and bring about parallelization by using a hypergraph partitioning algorithm and a two level hybrid parallel model. The whole computing domain is decomposed into sev
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Ilyakova, Anastasia V., Anzhelika S. Gonchar, Natalya I. Eremeeva, and Yulia V. Demina. "Assessment of efficiency of sanitary treatment of technological equipment at meat processing industry enterprise." Hygiene and sanitation 103, no. 7 (2024): 712–17. http://dx.doi.org/10.47470/0016-9900-2024-103-7-712-717.

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Introduction. To assess the efficiency of sanitary treatment of technological equipment at the meat processing industry enterprise, the assessment of microbial contamination of technological equipment surfaces after washing and disinfection with subsequent assessment of sensitivity of isolates of microorganisms to the used disinfectant was carried out. Material and methods. Washes from the surfaces of technological equipment were studied at the one of domestic meat-processing enterprises engaged in the production of sausage and semi-finished products from incoming meat raw materials (beef, por
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Mobley, Frank, and Steven Campbell. "Validation of acoustic directivity patterns from static and dynamic flight measurements." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 264, no. 1 (2022): 174–87. http://dx.doi.org/10.3397/nc-2022-711.

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Two methods have been proposed to measure the acoustic emissions for small unmanned aircraft systems (UAS): 1) dynamic flight through an outdoor microphone array, and 2) static test cell measurements. Both methods produce source directivity patterns for predicting levels where recordings had been made during dynamic flights. In autonomous flight the engine rotations-per-minute (RPM) are constantly adjusting to maintain the commanded aircraft airspeed and altitude. This violates the assumptions of stationality in acoustic emissions over a single pass that are inherent in the dynamic flight meth
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Mack, Andrew L. "Tundra to Tropics: Connecting Birds, Habitats and People.— Terrell D. Rich , Coro Arizmendi , Dean W. Demarest and Craig Thompson (editors). 2009 Proceedings of the 4th International Partners in Flight Conference, 13–16 February 2008, McAllen, Texas. Partners in Flight. 712 pp., paper; volume currently available only online at http://www.partnersinflight.org/pubs/McAllenProc/index.cfm." Condor 113, no. 2 (2011): 470–71. http://dx.doi.org/10.1525/cond.2011.113.2.470.

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Benson, Nicholas H., Roy L. Alson, Eve G. Norton, Ann P. Beauchamp, Rita Weber, and Jorge L. Carreras. "Air Medical Transport Utilization Review in North Carolina." Prehospital and Disaster Medicine 8, no. 2 (1993): 133–37. http://dx.doi.org/10.1017/s1049023x00040206.

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AbstractObjective:To perform a review of the collective experience of all hospital-based helicopter ambulances in the state of North Carolina for compliance with utilization review criteria.Design:Flight records of the six members of the North Carolina Aeromedical Affiliation for the months of November and December 1989 were compared with utilization review criteria by an independent reviewer. A secondary review was performed by a staff member for each service. Scene responses and patients flown to a hospital other than the sponsor were evaluated.Setting:All six hospital-based helicopter servi
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Nilssen, Arne C., and John R. Anderson. "Flight capacity of the reindeer warble fly, Hypoderma tarandi (L.), and the reindeer nose bot fly, Cephenemyia trompe (Modeer) (Diptera: Oestridae)." Canadian Journal of Zoology 73, no. 7 (1995): 1228–38. http://dx.doi.org/10.1139/z95-147.

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The performance of tethered flies on a laboratory flight mill was used to assess the flight capacity of Hypoderma tarandi (L.) and Cephenemyia trompe (Modeer). Maximum total flying times for H. tarandi females were 31.5 h, but most flies flew < 20 h (mean 8.5 h (SD 7.2 h)). The longest continuous flight was 12 h. For both species, mating greatly altered the flight behaviour of females. Unmated laboratory-reared females were reluctant to fly, and flew less continuously than mated wild-caught flies. Hypoderma tarandi males typically flew for short periods of a few minutes with long rests betw
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Atiković, Almir. "New Regression Models to Evaluate the Relationship between Biomechanics of Gymnastic Vault and Initial Vault Difficulty Values." Journal of Human Kinetics 35, no. 1 (2012): 119–26. http://dx.doi.org/10.2478/v10078-012-0085-6.

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The main objective of this paper was to determine the relationship between biomechanical parameters of vault flights with respect to new models of initial vault difficulty values in men’s artistic gymnastic. The study sample included vaults (n=64) and models (n=5) from the 2009 Code of Points (CoP) of the Federation International of Gymnastics (FIG). The dependent variable included all difficulty values ranging from 2-7.2 points, while the sample of independent variables included twelve biomechanical parameters. After implementing the regression analysis, it could be established that the best
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Dissertations / Theses on the topic "Flight 712"

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Borra, Brian M. "Nonlinear UAV Flight Control Using Command Filtered Backstepping." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/713.

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The aim of this effort is to implement a nonlinear flight control architecture, specifically flight path control via command filtered backstepping, for use in AME UAS's Fury® 1500 unmanned flying wing aircraft. Backstepping is a recursive, control-effort minimizing, constructive design procedure that interlaces the choice of a Lyapunov function with the design of feedback control. It allows the use of certain plant states to act as intermediate, virtual controls, for others breaking complex high order systems into a sequence of simpler lower-order design tasks. Work herein is a simplified impl
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Van, Nuffel Sebastiaan. "Three-dimensional time-of-flight secondary ion mass spectrometry imaging of primary neuronal cell cultures." Thesis, University of Nottingham, 2017. http://eprints.nottingham.ac.uk/39644/.

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Time-of-flight secondary ion mass spectrometry (ToF-SIMS) has proven its ability to characterise (in)organic surfaces, and is increasingly used for the characterisation of biological samples such as single cells. By combining ion imaging and molecular depth profiling it is possible to render 3D chemical images, which provides a novel, label-free way to investigate biological systems. Major challenges lie, however, in the development of data analysis tools and protocols that preserve the cell morphology. Here, we develop and employ such tools and protocols for the investigation of neuronal netw
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Cetin, Yasemin. "Evaluation Of Visual Cues Of Three Dimensional Virtual Environments For Helicopter Simulators." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/2/12610100/index.pdf.

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Flight simulators are widely used by the military, civil and commercial aviation. Visual cues are an essential part of helicopter flight. The required cues for hover are especially large due to closeness to the ground and small movements. In this thesis, density and height parameters of the 3D (Three Dimensional) objects in the scene are analyzed to find their effect on hovering and low altitude flight. An experiment is conducted using a PC-based flight simulator with three LCD monitors and flight control set. Ten professional military pilots participated in the experiment. v Results revealed
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MacLennan, H. A. "A study of the performance of office workers descending multiple flights of stairs in high rise office buildings in trial evacuations." Thesis, University of Salford, 2013. http://usir.salford.ac.uk/29452/.

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Aim: The Aim of this PhD study is to study the performance of mature age office workers descending multiple flights of stairs in trial evacuations of high rise office buildings in the context of extrinsic and intrinsic factors. Method: A case study process coupled with mixed methods data collection and analysis was selected with the unit of analysis being the office worker descending the stairs. An Exploratory case study involving the reanalysis of data from a similar study was undertaken to confirm the selection of the research method. Six high rise buildings were selected varying from 7 to 3
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Daouayry, Nassia. "Détection d’évènements anormaux dans les gros volumes de données d’utilisation issues des hélicoptères." Thesis, Lyon, 2020. http://www.theses.fr/2020LYSEI084.

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Cette thèse aborde le sujet de la normalité de fonctionnement des systèmes composants l’hélicoptère à travers l’exploitation des données d’utilisation issues du système de surveillances du HUMS (Health and Usage Monitoring System) pour la maintenance. Les hélicoptères sont des systèmes complexes et sont soumis à des exigences réglementaires strictes imposées par les autorités concernées par la sécurité en vol. L’analyse des données de surveillance est par conséquent un moyen privilégié pour améliorer la maintenance des hélicoptères. De plus, les données produites par le système HUMS représente
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Books on the topic "Flight 712"

1

Ottaway, Susan. Fire over Heathrow: The tragedy of flight 712. Pen & Sword Aviation, 2008.

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Hergé. Flight 714. Mammoth, 1989.

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F, Seible, and United States. National Aeronautics and Space Administration., eds. NASTRAN modeling of flight test components for UH-60A airloads program test configuration: Final report on a research project funded through NASA research grant number NCC2-712. Dept. of Applied Mechanics and Engineering Sciences, University of California, San Diego, 1993.

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1945-, Goodall James C., ed. SR-71 pilot's manual: The official US Air Force SR-71A flight manual. Motorbooks International, 1992.

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Dante, Jackson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Supersonic flying qualities experience using the SR-71. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Hwei-Lan, Chou, and United States. National Aeronautics and Space Administration., eds. Low bandwidth robust controllers for flight: NASA Grant NCC 2-711, June 1991 - December 1992, final report. National Aeronautics and Space Administration, 1993.

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J, Ehernberger L., Whitmore Stephen A, and Dryden Flight Research Facility, eds. Preliminary airborne measurements for the SR-71 sonic boom propagation experiment. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.

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J, Ehernberger L., Whitmore Stephen A, and Dryden Flight Research Facility, eds. Preliminary airborne measurements for the SR-71 sonic boom propagation experiment. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.

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Merlin, Peter W. Mach 3+: NASA/USAF YF-12 flight research, 1969-1979. NASA History Division, Office of External Affairs, NASA Headquarters, 2002.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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Book chapters on the topic "Flight 712"

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Moseley, M. A. "Coaxial Nanospray Coupled with a Hybrid Quadrupole/Time-of-Flight Tandem Mass Spectrometer for Proteome Studies." In Mass Spectrometry in Biology & Medicine. Humana Press, 2000. http://dx.doi.org/10.1007/978-1-59259-719-2_11.

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Krutchinsky, A. N., I. V. Chernushevich, A. V. Loboda, W. Ens, and K. G. Standing. "Measurements of Protein Structure and Noncovalent Interactions by Time-of-Flight Mass Spectrometry with Orthogonal Ion Injection." In Mass Spectrometry in Biology & Medicine. Humana Press, 2000. http://dx.doi.org/10.1007/978-1-59259-719-2_2.

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Xie, Jiaqiang, and Wei Kuang. "Simulation of the Mixing Performance of an Optimized Air Injector." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-7887-4_99.

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Abstract The trim air system is an important system for realizing the temperature control of the flight deck and passenger cabin of commercial aircraft. The trim air duct is designed to bleed the high-temperature air to mix the cold air from the upstream of the refrigeration components in order to satisfy the independent temperature requirements of each area of the flight deck and passenger cabin. If the cold air and hot air mixing situation was poor, downstream temperature sensor layout location there is still a more serious hot and cold air stratification, the measured value is more difficul
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Wong, Kenneth. "Developing commercial human space-flight regulations." In Space Safety Regulations and Standards. Elsevier, 2010. http://dx.doi.org/10.1016/b978-1-85617-752-8.10013-3.

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Lomas, Daniel W. B. "Introduction." In Intelligence, Security and the Attlee Governments, 1945-51. Manchester University Press, 2017. http://dx.doi.org/10.7228/manchester/9780719099144.003.0001.

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Clement Richard Attlee, the Labour Party’s longest serving leader and Prime Minister during an unprecedented period of change for Britain, stands in the ‘top flight’ of post-war premiers.<sup>1</sup> A poll of MPs in 2015, seventy years after Labour’s first ever majority in Parliament, rated Attlee as the greatest post-war prime minister, with an average score of 7.2 out of 10 for overall impact....
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Sgobba, Tommaso, and Joseph N. Pelton. "Certification of new experimental commercial human space-flight vehicles." In Space Safety Regulations and Standards. Elsevier, 2010. http://dx.doi.org/10.1016/b978-1-85617-752-8.10008-x.

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Pelton, Joseph N. "The international challenges of regulation of commercial space flight." In Space Safety Regulations and Standards. Elsevier, 2010. http://dx.doi.org/10.1016/b978-1-85617-752-8.10023-6.

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Hayrapetyan Narek, Hakobyan Robert, Poghosyan Aghasy, and Gabrielyan Vazgen. "Border Surveillance Using UAVs with Thermal Camera." In NATO Science for Peace and Security Series - D: Information and Communication Security. IOS Press, 2016. https://doi.org/10.3233/978-1-61499-716-0-219.

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Unmanned Aerial Vehicles (UAVs) provide an opportunity to make 24/7 surveillance possible in large areas of strategic importance such as industrial plants and borders. In this paper we present an algorithm for detecting people in surveillance areas in low visibility conditions. The efficiency of the current solution is based on using an onboard thermal camera as a sensor, which generates a heat map even at nighttime and in bad weather. UAV flight details and technical characteristics are also discussed.
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Hugo, Noubel, and Viviana Lago. "Experimental Analysis of Waverider Lift-to-Drag Ratio Measurements in Rarefied and Supersonic Regime." In Hypersonic Vehicles - Applications, Recent Advances, and Perspectives [Working Title]. IntechOpen, 2021. http://dx.doi.org/10.5772/intechopen.100328.

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This work, performed in the MARHY rarefied hypersonic facility, experimentally explores the effects of rarefaction on a classical waverider geometry. This hypersonic vehicle is designed to develop a shock attached along the leading edge length to improve flight efficiency. The concept was first proposed by Nonweiler in 1959. Since then, many studies have been conducted, mainly on numerical aspects. Few works have included the influence of the viscous effect, we can cite those of Bowcutt who showed how viscous effects impact the optimal shapes due to the skin friction drag. However, the traject
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Chan, Joseph, and Richard DalBello. "Data sharing to improve close approach monitoring and safety of flight." In Space Safety Regulations and Standards. Elsevier, 2010. http://dx.doi.org/10.1016/b978-1-85617-752-8.10011-x.

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Conference papers on the topic "Flight 712"

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Zaman, Tanzina, and Abdel Bayoumi. "Estimation of Economic Effectiveness of HUMS Equipped AH-64 Aircraft: An ROI Approach." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11516.

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Cost-benefit analysis has always been a prime requirement to demonstrate the success of Condition-based Maintenance (CBM) practice in Army rotorcraft (Apache, Blackhawk, Kiowa, and Chinook, etc.). This study investigates whether the benefit of CBM practice in AH-64 aircraft over a 14-year period overweighs the investment cost. The benefit is calculated in terms of direct cost and operating cost analyzing maintenance logs and flight records. Direct cost is calculated in monetary value but operating cost is first calculated in hours and then converted into a monetary value. The direct and operat
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Mula, Swathi, Christopher Cameron, Charles Tinney, and Jayant Sirohi. "Low-dimensional Characteristics of Tip Vortices from a Coaxial Rotor in Hover." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9438.

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PIV experiments are conducted on a coaxial rotor wake to study the low-dimensional characteristics of the turbulence within the rotor tip vortices using proper orthogonal decomposition (POD). The coaxial configuration consists of 1.0 m diameter, two-bladed twin rotors spaced at 15% radius. The coaxial rotor is operated in hover at a blade tip chord Reynolds number of 218,000 and a tip Mach number of 0.23. Blades are set to collective pitch angles of 7.1° (upper rotor) and 7.2° (lower rotor), all of which resulted in a blade loading CT ₙ/σ = 0.035 with a sufficient torque balance. Corrections f
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Schatzman, Natasha, Athena Chan, Michael Fillman, et al. "Performance Analysis and Data Processing for the Mars Sample Recovery Helicopter in the Jet Propulsion Laboratory 25-ft Space Simulator." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1357.

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On April 19, 2021, Ingenuity became the first helicopter to fly on Mars at Jezero Crater, completing a total of 72 flights by the end of its mission. The success of Ingenuity resulted in various research efforts to further exploreMars via vertical flight, including two optimized Ingenuity-sized helicopters proposed to retrieve samples for the 2028 Mars Sample Return mission. To aid in the design process for the two proposed Sample Retrieval Helicopters, both heritage and optimized, increased diameter rotors were tested at the NASA Jet Propulsion Laboratory in the 25-ft Space Simulator. Three t
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Connolly, Kevin, Marc Tardiff, and George Matook. "Development of a Helicopter Sling Load Unmanned Hookup Device." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12213.

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Helicopter Sling Load (HSL) missions pose significant safety risks to the ground personnel involved with hooking up payloads to the helicopter. The goal of this project is to develop a materiel solution to increase the safety of an HSL hookup team by eliminating the personnel subjected to the hazards of the HSL mission. The research reviewed in this paper discusses two concepts that were evaluated for HSL auto hookup capabilities: a grapple hook design with three spring articulating arms and a system that used a cone on cone design. For this project, flight evaluations were conducted on protot
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Singh, Rajneesh, Michael Avera, Hao Kang, and Matthew Floros. "Technology Identification for a High Performance Tailsitter VTOL Aircraft." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9430.

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A sensitivity study on the performance of a 10,000 lb, dual rotor tailsitter aircraft was conducted. A data set of 72 unique configurations was constructed using manual design space exploration, a screening design of experiments, and a response surface design of experiments. The performance of each configurations was analyzed using the FLIGHTLAB rotorcraft simulation software for low speed flight from 0–100 kts and high speed flight from 150-300 kts. The resulting data was used to construct eleven surrogate performance models using the JMP statistical analysis software. The sensitivity of the
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Stevens, Mark, Mark Valco, and Kelsen LaBerge. "Two-Speed Rotorcraft Research Transmission Power-Loss Associated with the Lubrication and Hydraulic Rotating Feed-Through Design Feature." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12853.

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An investigation was completed into the power loss associated with a rotating feed-through (RFT) design feature used to transfer lubrication and a hydraulic control signal from the static reference frame to a rotating reference frame in the NASA GRC two-speed transmission tests conducted in the Variable-Speed Drive Test Rig. The RFT feature, not commercially available, was created specifically for this research project and is integral to all two-speed transmission configurations tested, as well as a variant concept design for a geared variable-speed transmission presented at AHS Forum 71 in 20
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Gaugelhofer, Lucas, Jonas John, Manfred Hajek, and Likay Yavrucuk. "Lightning Strike Experiments and Their Direct Effects on Flax Fiber-Reinforced Polymer Panels for Rotorcraft Components." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1307.

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This paper experimentally investigates direct effects of lightning strikes on flax fiber-reinforced polymers. Highcurrent artificial lightning strikes are conducted on coupon level to evaluate thermo-mechanical damage and to quantify the sufficiency of copper wire mesh as lightning strike protection (LSP). The dataset shall also serve for verification of prospected numerical simulation. The natural fiber flax, as a sustainable source of composite reinforcement, has been demonstrated to be suitable for semi-structural parts of rotorcraft. However, its low electrical and thermal conductivity req
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Swales, C., G. Breeze, C. Swales, and G. Breeze. "LDV measurements above the flight deck of a model frigate." In 35th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-712.

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Gupta, Kajal, Leonard Voelker, Can Bach, Timothy Doyle, and Edward Hahn. "CFD-based aeroelastic analysis of the X-43 hypersonic flight vehicle." In 39th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-712.

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Robson, Geoffrey, and Raffaello D'Andrea. "Longitudinal Stability Analysis of a Jet-Powered Wingsuit." In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-7512.

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Reports on the topic "Flight 712"

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Marcot, Bruce, M. Jorgenson, Thomas Douglas, and Patricia Nelsen. Photographic aerial transects of Fort Wainwright, Alaska. Engineer Research and Development Center (U.S.), 2022. http://dx.doi.org/10.21079/11681/45283.

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This report presents the results of low-altitude photographic transects conducted over the training areas of US Army Garrison Fort Wainwright, in the boreal biome of central Alaska, to document baseline land-cover conditions. Flights were conducted via a Cessna™ 180 on two flight paths over portions of the Tanana Flats, Yukon, and Donnelly Training Areas and covered 486 mi (782 km) while documenting GPS waypoints. Nadir photographs were made with two GoPro™ cameras operating at 5 sec time-lapse intervals and with a handheld digital camera for oblique imagery. This yielded 6,063 GoPro photos an
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