Power calculations for isentropic compressions of cryogenic nitrogen

A theoretical analysis has been made of the power required for isentropic compressions of cryogenic nitrogen in order to determine the extent that the drive power for cryogenic tunnels might be affected by real gas effects. The analysis covers temperatures from 80 to 310K, pressures from 1.0 to 8.8 atm and fan pressure ratios from 1.025 to 1.200. The power required to compress cryogenic nitrogen was found to be lower than that required for an ideal diatomic gas by as much as 9.5 percent. Simple corrections to the ideal gas values were found to give accurate estimates of the real gas power values

Power calculations for isentropic compressions of cryogenic nitrogen

A theoretical analysis was made of the power required for isentropic compressions of cryogenic nitrogen in order to determine the extent to which the drive power for cryogenic tunnels might be affected by real-gas effects. The analysis covers temperatures from 80 to 310 K, pressures from 1.0 to 8.8 atm, and fan pressure ratios from 1.025 to 1.200. The power required to compress cryogenic nitrogen was found to be as much as 9.5 percent lower than that required to compress an ideal diatomic gas. Simple corrections to the ideal-gas values were found to give accurate estimates of the real-gas power values

Exploratory piloted simulator study of the effects of winglets on handling qualities of a representative agricultural airplane

The effects on handling qualities of adding winglets to a representative agricultural aircraft configuration during swath-run maneuvering were evaluated. Aerodynamic data used in the simulation were based on low-speed wind tunnel tests of a full scale airplane and a subscale model. The Cooper-Harper handling qualities rating scale, supplementary pilot comments, and pilot vehicle performance data were used to describe the handling qualities of the airplane with the different wing-tip configurations. Results showed that the lateral-directional handling qualities of the airplane were greatly affected by the application of winglets and winglet cant angle. The airplane with winglets canted out 20 deg exhibited severely degraded lateral directional handling qualities in comparison to the basic airplane. When the winglets were canted inward 10 deg, the flying qualities of the configuration were markedly improved over those of the winglet-canted-out configuration or the basic configuration without winglets, indicating that proper tailoring of the winglet design may afford a potential benefit in the area of handling qualities

Control-system techniques for improved departure/spin resistance for fighter aircraft

Some fundamental information on control system effects on controllability of highly maneuverable aircraft at high angles of attack are summarized as well as techniques for enhancing fighter aircraft departure/spin resistance using control system design. The discussion includes: (1) a brief review of pertinent high angle of attack phenomena including aerodynamics, inertia coupling, and kinematic coupling; (2) effects of conventional stability augmentation systems at high angles of attack; (3) high angle of attack control system concepts designed to enhance departure/spin resistance; and (4) the outlook for applications of these concepts to future fighters, particularly those designs which incorporate relaxed static stability

Topological Quantum Computing with Only One Mobile Quasiparticle

In a topological quantum computer, universal quantum computation is performed by dragging quasiparticle excitations of certain two dimensional systems around each other to form braids of their world lines in 2+1 dimensional space-time. In this paper we show that any such quantum computation that can be done by braiding $n$ identical quasiparticles can also be done by moving a single quasiparticle around n-1 other identical quasiparticles whose positions remain fixed.Comment: 4 pages, 5 figure

The NSW Oyster Industry: A Risk Indicator of Sustainable Coastal Policy and Practice

Estuaries are the 'door mat' of human activity on land. They are also highly valued by the community. The New South Wales (NSW) oyster industry is Australia's oldest farming enterprise, dating back to the pre-European settlement era and as a consequence has social and cultural significance. Oyster farmers have developed generations of understanding and professional and intimate observation of the subtleties and frailties of NSW estuaries, cultivating their shells on a daily basis. The key motivation for this study is that the NSW oyster industry is a risk indicator of sustainable coastal catchment policy and practice. The studies are based on the overarching hypothesis that the economic, social, cultural, human health and environmental sustainability objectives of the NSW oyster industry require a historically- and scientifically-based risk analysis framework for selecting, managing and cultivating oyster farming areas. A review identified that it was vulnerable because of the lack of protection and planning for oyster growing areas. The aim of this thesis is to demonstrate that policies based on a risk analysis framework optimise outcomes for strategic management of the NSW oyster industry where risk is defined in terms of the effect of uncertainties on the industry's economic, social, cultural, human health and environmental sustainability objectives. The results demonstrate that a risk-based framework is effective in developing policy in strategic management of the NSW oyster industry and reducing uncertainty for the industry's economic, social, cultural, human health and environmental sustainability objectives. New approaches to improving profitability and durability and reducing risk to the NSW oyster industry objectives have been implemented as policy outcomes and industry practices as a result of this approach. Research and governance issues and the establishment of a management framework that fosters strategic policy development based on sound science using risk analysis and priority setting are all important steps on the ladder of estuarine ecosystem conservation and recovery. The policy outcomes that have been implemented in NSW as a result of a risk-based strategic approach are practical, tactical and goal oriented with the oyster industry recognised up-front in land use planning to address the consequences of potential impacts from ongoing rapid coastal urbanisation. A key element is the NSW Oyster Industry Sustainable Aquaculture Strategy

Braid Topologies for Quantum Computation

In topological quantum computation, quantum information is stored in states which are intrinsically protected from decoherence, and quantum gates are carried out by dragging particle-like excitations (quasiparticles) around one another in two space dimensions. The resulting quasiparticle trajectories define world-lines in three dimensional space-time, and the corresponding quantum gates depend only on the topology of the braids formed by these world-lines. We show how to find braids that yield a universal set of quantum gates for qubits encoded using a specific kind of quasiparticle which is particularly promising for experimental realization.Comment: 4 pages, 4 figures, minor revision

Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability

A real-time piloted simulation was conducted to evaluate the high-angle-of-attack characteristics of a fighter configuration based on wind-tunnel testing of the F-16, with particular emphasis on the effects of various levels of relaxed longitudinal static stability. The aerodynamic data used in the simulation was conducted on the Langley differential maneuvering simulator, and the evaluation involved representative low-speed combat maneuvering. Results of the investigation show that the airplane with the basic control system was resistant to the classical yaw departure; however, it was susceptible to pitch departures induced by inertia coupling during rapid, large-amplitude rolls at low airspeed. The airplane also exhibited a deep-stall trim which could be flown into and from which it was difficult to recover. Control-system modifications were developed which greatly decreased the airplane susceptibility to the inertia-coupling departure and which provided a reliable means for recovering from the deep stall