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  • 1
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    Low-Cost Methods for Molecular Characterization of Mutant Plants : Tissue Desiccation, DNA Extraction and Mutation Discovery: Protocols (2015)
    Cham : Springer
    Details
    Keywords: Life sciences ; Nucleic acids ; Plant breeding ; Biology ; Technique ; Life Sciences ; Plant Breeding/Biotechnology ; Biological Techniques ; Nucleic Acid Chemistry
    Description / Table of Contents: Introduction --- Health and Safety Considerations --- Sample Collection and Storage --- Low-Cost DNA Extraction --- PCR Amplification for Low-Cost Mutation Discovery --- Enzymatic Mismatch Cleavage and Agarose Gel Evaluation of Samples --- Alternative Enzymology for Mismatch Cleavage for TILLING and Ecotilling: Extraction of Enzymes form Common Weedy Plants --- Example Data --- Conclusions.  
    Pages: Online-Ressource (X, 35 pages) , 9 illustrations, 3 illustrations in color
    ISBN: 9783319162591
    URL: https://link.springer.com/openurl?genre=book&isbn=978-3-319-16259-1
    Language: English
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    E-BOOK
  • 2
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    Low-Cost Methods for Molecular Characterization of Mutant Plants (2021)
    Springer Nature
    Details
    Publication Date: 2023-03-03
    Description: Plant Breeding/Biotechnology; Biological Techniques; Nucleic Acid Chemistry
    Keywords: Plant Breeding/Biotechnology ; Biological Techniques ; Nucleic Acid Chemistry ; bic Book Industry Communication::K Economics, finance, business & management::KN Industry & industrial studies::KND Manufacturing industries ; bic Book Industry Communication::K Economics, finance, business & management::KN Industry & industrial studies::KND Manufacturing industries::KNDP Pharmaceutical industries ; bic Book Industry Communication::T Technology, engineering, agriculture::TC Biochemical engineering
    Language: English
    Format: image/jpeg
    Format: image/jpeg
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    E-BOOK
  • 3
    Electronic Resource
    Electronic Resource
    On the morphology of oriented nylon-12 (1985)
    Springer
    Colloid & polymer science 263 (1985), S. 116-119 
    Details
    ISSN: 1435-1536
    Keywords: Electron microscopy ; staining ; morphology ; nylon-12 ; orientation
    Source: Springer Online Journal Archives 1860-2000
    Topics: Chemistry and Pharmacology , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The morphology of drawn and annealed sheets of nylon-12 was investigated by transmission electron microscopy of stained sections, and the results compared with equivalent small-angle X-ray scattering (SAXS) patterns. A three-component structure was observed, consisting of crystalline (C) and amorphous (A) regions in the microfibrils and an interfibrillar component whose density was deduced to be intermediate between that of the C and A regions. The crystallite width was given satisfactorily by a Guinier analysis of the SAXS profile.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01412785
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    Paper (German National Licenses)
    Fulltext
  • 4
    Electronic Resource
    Electronic Resource
    Orientation in low-density polyethylene due to an elementary slip process (1988)
    Springer
    Colloid & polymer science 266 (1988), S. 311-315 
    Details
    ISSN: 1435-1536
    Keywords: Low-densitypolyethylene ; orientation ; slip process ; birefringence ; mechanicalanisotropy
    Source: Springer Online Journal Archives 1860-2000
    Topics: Chemistry and Pharmacology , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract A simple, physical model has been developed to describe orientation in thermoplastic polymers, involving the boundary slip and rotation of rod-like structural elements. Orientation parameters have been calculated, and expressions for the birefringence and elastic mechanical anisotropy deduced. Results on cold-drawn, low-density polyethylene agree well with this model.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01451813
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    Paper (German National Licenses)
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  • 5
    Electronic Resource
    Electronic Resource
    Electron microscopy of oriented high-density polyethylene: Comparison with small-angle X-ray scattering (1984)
    Springer
    Colloid & polymer science 262 (1984), S. 793-797 
    Details
    ISSN: 1435-1536
    Keywords: electron microscopy ; polyethylene ; morphology ; orientation ; small-angle X-ray scattering
    Source: Springer Online Journal Archives 1860-2000
    Topics: Chemistry and Pharmacology , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The morphology of cold-drawn, rolled and annealed high-density polyethylene was investigated by transmission electron microscopy of stained sections. From the electron micrographs, a model of the structure was developed and the scattering pattern calculated. This was then compared with the corresponding small-angle X-ray scattering (SAXS) pattern, in order both to aid in the interpretation of SAXS patterns of oriented polymers, and to assess the effects of staining with chlorosulphonic acid on the morphology.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01451709
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    Paper (German National Licenses)
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  • 6
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    Comparisons Between Unsteady Aerodynamic Events in a Gas Turbine Generator and an Identical Compressor Rig (1996)
    In:  CASI
    Details
    Publication Date: 2011-10-14
    Description: Extensive testing done on a T55-L-712 turboshaft engine compressor in a compressor test rig is being followed by engine tests in progress as part of the Army Non-Recoverable Stall Program. Goals include a greater understanding of the gas turbine engine start cycle and compressor/engine operation in the regions 'beyond' the normal compressor stall line (rotating stall/surge). Rig steady state instrumentation consisted of 497 steady state pressure sensors and 153 temperature sensors. Engine instrumentation was placed in similar radial/axial locations and consists of 122 steady state pressure sensors and 65 temperature sensors. High response rig instrumentation consisted of 34 wall static pressure transducers. Rig and engine high response pressure transducers were located in the same axial/radial/circumferential locations in front of the first three stages. Additional engine high response instrumentation was placed in mach probes in front of the engine and on the compressor hub. This instrumentation allows for the generation of detailed stage characteristics, overall compressor mapping, and detailed analysis of dynamic compressor events.
    Keywords: Aircraft Propulsion and Power
    Type: Loss Mechanisms and Unsteady Flows in Turbomachines; AGARD-CP-571
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    Space Transportation Propulsion Systems (2001)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: This report outlines the Space Transportation Propulsion Systems for the NPSS (Numerical Propulsion System Simulation) program. Topics include: 1) a review of Engine/Inlet Coupling Work; 2) Background/Organization of Space Transportation Initiative; 3) Synergy between High Performance Computing and Communications Program (HPCCP) and Advanced Space Transportation Program (ASTP); 4) Status of Space Transportation Effort, including planned deliverables for FY01-FY06, FY00 accomplishments (HPCCP Funded) and FY01 Major Milestones (HPCCP and ASTP); and 5) a review current technical efforts, including a review of the Rocket-Based Combined-Cycle (RBCC), Scope of Work, RBCC Concept Aerodynamic Analysis and RBCC Concept Multidisciplinary Analysis.
    Keywords: Aircraft Propulsion and Power
    Type: 2000 Numerical Propulsion System Simulation Review; 59-69; NASA/CP-2001-210673
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Validation of an Integrated Airframe and Turbofan Engine Simulation for Evaluation of Propulsion Control Modes (2015)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The National Aeronautics and Space Administration (NASA) has developed independent airframe and engine models that have been integrated into a single real-time aircraft simulation for piloted evaluation of propulsion control algorithms. In order to have confidence in the results of these evaluations, the integrated simulation must be validated to demonstrate that its behavior is realistic and that it meets the appropriate Federal Aviation Administration (FAA) certification requirements for aircraft. The paper describes the test procedures and results, demonstrating that the integrated simulation generally meets the FAA requirements and is thus a valid testbed for evaluation of propulsion control modes.
    Keywords: Aircraft Propulsion and Power
    Type: GRC-E-DAA-TN19726 , SciTech 2015; Jan 05, 2015 - Jan 09, 2015; Kissimmee, FL; United States
    Format: application/pdf
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  • 9
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    Flight Simulator Evaluation of Enhanced Propulsion Control Modes for Emergency Operation (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper describes piloted evaluation of enhanced propulsion control modes for emergency operation of aircraft. Fast Response and Overthrust modes were implemented to assess their ability to help avoid or mitigate potentially catastrophic situations, both on the ground and in flight. Tests were conducted to determine the reduction in takeoff distance achievable using the Overthrust mode. Also, improvements in Dutch roll damping, enabled by using yaw rate feedback to the engines to replace the function of a stuck rudder, were investigated. Finally, pilot workload and ability to handle the impaired aircraft on approach and landing were studied. The results showed that improvement in all aspects is possible with these enhanced propulsion control modes, but the way in which they are initiated and incorporated is important for pilot comfort and perceived benefit.
    Keywords: Aircraft Propulsion and Power
    Type: NASA/TM-2012-217698 , AIAA Paper 2012-2604 , E-18385 , AIAA Infotech@Aerospace Conference; Jun 19, 2012 - Jun 21, 2012; Garden Grove, CA; United States
    Format: application/pdf
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  • 10
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    An Intelligent Propulsion Control Architecture to Enable More Autonomous Vehicle Operation (2017)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper describes an intelligent propulsion control architecture that coordinates with the flight control to reduce the amount of pilot intervention required to operate the vehicle. Objectives of the architecture include the ability to: automatically recognize the aircraft operating state and flight phase; configure engine control to optimize performance with knowledge of engine condition and capability; enhance aircraft performance by coordinating propulsion control with flight control; and recognize off-nominal propulsion situations and to respond to them autonomously. The hierarchical intelligent propulsion system control can be decomposed into a propulsion system level and an individual engine level. The architecture is designed to be flexible to accommodate evolving requirements, adapt to technology improvements, and maintain safety.
    Keywords: Aircraft Propulsion and Power
    Type: GRC-E-DAA-TN50405 , SciTech 2018; Jan 08, 2018 - Jan 12, 2018; Kissimmee, FL; United States
    Format: application/pdf
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