11 research outputs found
The PSHPP Chebren and Galishte opportunity for rehabilitation of Mariovo – Macedonia
- Publication venue
- 'Informa UK Limited'
- Publication date
- Field of study
A Study of Airplane Excrescence Drag
- Author
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Lunar flying vehicle propulsion system
- Author
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Advancved Tactical Missile
- Author
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Bibliography
- Author
- Abgasturboaufladung Thermodynamische Untersuchungen
- Aeroplane Performances
- Air Cooled A Preliminary Investigation
- Airplane Engine Supercharging
- Airplanes The Calculated
- Altitude
- An
- An
- Aviation Le Moteur
- Aviation Les Compresseurs
- Aviation Suralimentation
- Basses Altitudes Note Sur
- Centrifugal Compressors Surging
- Centrifugal Supercharger Influence
- Combustion Suralimentation
- Critical The
- Dimensional The Application
- Electric The General
- Engines A New Deal
- Engines Supercharged Aero
- Espace Note
- Etude des Roues Contribution
- Examen des Realisations Les Problemes
- Flight Comparative
- Flight Preliminary
- Hochleistungsmotoren Ladeeinrichtungen
- Influence
- La
- Laboratory Description
- Les Compresseurs
- Les Compresseurs Volumetriques Les Problemes
- Les Problemes
- Performance Calculated Supercharged Engine
- Powerplus Vane-Type Supercharger Comparative Performance
- Problems Supercharger Installation
- Ricerche
- Solution Une
- Some Experiments
- Some Supercharger
- Supercharged Aircraft Design
- Supercharged Engine A
- Supercharger Airplane
- Superchargers
- Superchargers The Comparative
- Sur
- The
- The
- The
- The
- Valve The Effect
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Construction of Cis-Cyclopropane Structure via Reductive Radical Decarboxylation. Enantioselective Synthesis of Cis- and Trans-1-arylpiperazyl-2-phenylcyclopropanes Designed as Antidopaminergic Agents
- Author
- Apeloig Y.
- Barton D. H. R.
- Barton D. H. R.
- Chatgilialoglu C.
- Curran D. P.
- Cyclopropyl
- Drug Design
- DĂaz-Requejo M. M.
- For
- For
- For
- For
- Frisch M. J.
- Isobe M.
- Kanabus-Kaminska J. M.
- Kaye P. T.
- Kazuta Y.
- Kazuta Y.
- Kazuta Y.
- Nahn S.
- Niimi T.
- Preliminary
- Renaud
- Reviews
- Sasaki T.
- Shuto S.
- Sibley D. R.
- Silverman R. B.
- Stammer S. H.
- The Dopamine Receptors
- The Practice
- Toy P. H.
- Walborsky H. M.
- Wong H. N. C.
- Zhang M.-X.
- Zhang X.
- Publication venue
- 'American Chemical Society (ACS)'
- Publication date
- Field of study
Observation Unit Management of Heart Failure
- Author
- Albert
- Ashton
- Baker
- Barjon
- Batsford
- Bristow
- Bristow
- Bumetadine
- Butman
- Chait
- Chakko
- CIBIS Investigators and Committees
- Cioffi
- Cohn
- Cohn
- Cohn
- Colucci
- Doval
- Elkayam
- Elkayam
- Francis
- Francis
- Ghali
- Goldstein
- Grossman
- Guidelines for the evaluation and management of heart failure
- Ho
- Hobbs
- Julian
- Koga
- Kono
- Krumholz
- Le Conte
- Loer
- Lubsen
- Marantz
- Massie
- McKee
- McKelvie
- Nancy M. Albert
- O'Connell
- O'Connor
- Packer
- Packer
- Packer
- Peacock
- Peacock
- Peacock
- Pitt
- Pitt
- Remes
- Rich
- Rich
- Ruskin
- Singh
- Stevenson
- Studies of left ventricular dysfunction (SOLVD)—rationale design and methods
- The Cardiac Arrhythmia Suppression Trail II Investigators
- The Cardiac Arrhythmia Suppression Trial (CAST) Investigators: Preliminary report
- The CONSENSUS Trial Study Group
- The Digitalis Investigation Group
- The International Steering Committee
- The SOLVD Investigators
- Tsuyuki
- Tsuyuki
- Van Lente
- Vinson
- William Franklin Peacock
- Publication venue
- 'Elsevier BV'
- Publication date
- Field of study
Current–Voltage Characteristics
- Author
- A Barone
- A Larkin
- A Schmid
- A Steinbach
- AB Zorin
- AD Whalen
- AW Kleinsasser
- AW Kleinsasser
- CL Foden
- CR Ast
- D Averin
- D Massarotti
- D Vion
- D. Massarotti
- DE McCumber
- DE Prober
- design and preliminary experimental results
- DG McDonald
- E Ben-Jacob
- E Scheer
- E Wolf
- EN Bratus’
- EV Bezuglyi
- F Tafuri
- G Schon
- G-L Ingold
- G-L Ingold
- G-L Ingold
- GB Arnold
- GE Blonder
- Gerald B. Arnold
- H Grabert
- H Nyquist
- H. Akoh
- HB Callen
- J Ankerhold
- J Ankerhold
- J Johnson
- J Kurkijarvi
- J Niemeyer
- J. C. Cuevas
- JI Pankove
- JM Martinis
- JM Martinis
- JP Heida
- JR Kirtley
- JR Waldram
- JW Wilkins
- K. Flensberg
- Kees M. Schep
- KK Likharev
- KK Likharev
- LE Hasselberg
- M Iansiti
- M Iansiti
- M Octavio
- M Tinkham
- M. BĂĽttiker
- M. Iansiti
- Melvin Lax
- MG Castellano
- N Post van der
- N. F. Pedersen
- NF Pedersen
- NR Werthamer
- P Dutta
- P Joyez
- PA Lee
- PK Hansma
- PK Hansma
- R Cristiano
- R Kummel
- R. Ono
- RE Miller
- RF Voss
- RH Koch
- RL Kautz
- RL Stratonovich
- Sh Kogan
- T. M. Klapwijk
- TA Fulton
- TD Clark
- Th. Martin
- U. Gunsenheimer
- V Ambegaokar
- V. Gubankov
- WC Scott
- WC Stewart
- WJ Tomasch
- WL McMillan
- Y Naveh
- Y Song
- YC Chen
- YM Lee
- Publication venue
- 'Springer Science and Business Media LLC'
- Publication date
- 01/01/2019
- Field of study
The physical processes occurring in junctions and weak links are encoded in their I–V characteristics. In this Chapter we discuss the main notions on the modeling of I–V curves with reference to the microscopic theory mostly applied to tunnel junctions, and to the Resistively Shunted Junction model, which provides appropriate tools to describe the enlarged family of weak links. Modeling I–V curves is the first step to define the transport mechanisms of a junction, its electrodynamics, and to understand its potential for applications in real circuits
Technical Literature Digest
- Author
- Aerodynamic Heat Transfer Measurement
- Aeronautical Sciences Progress
- Aerosols The Physical
- Airborne Missiles Underwater Launching
- Airborne Missiles Underwater Launching
- Airspeed Tables
- Arc Positive An Experimental
- Atomic
- Base On
- Charged Interaction
- Chemistry Temperature
- Diffuser Effects
- Dissociated Air Transport Properties
- Dissociation The Effect
- Distribution Pressure
- Distributions Approximate Temperature
- Electrically Conducting Fluid Heat Transfer
- Enthalpy Approximation
- Equilibrium Boundary Radiation Emission
- Equilibrium One-Dimensional Steady An Approximate
- Exact Some
- External Hypersonic Flows Chemical Effects
- Film An Approximate
- Flow Fields About Some A Study
- Free Shear-Layer Instability Some Aspects
- Free-Flight Supersonic
- Heat High Temperature
- Heat Transfer Boundary Layer
- Heat Transfer Local Aerodynamic
- Heat Transfer Similarity Modeling Technique
- Hemisphere Pressure Distributions
- Hydroand The Basic
- Hypersonic Flow Blunt Body
- Hypersonic Flows Axisymmetric Nozzles
- Hypersonic Rarefied Gas Flow A Kinetic Model
- Hypersonic Theoretical Prediction
- In-Flight Acoustic Ground
- Individual Gas Bubbles Mass Transfer
- Infrared Study
- Jet Laminar
- Kinetic On
- Laminar A Theory
- Layer Interaction Shock-Boundary
- Leading
- Lenticular-Shaped Reentry Landing Characteristics
- Magnetic Field The Interaction
- Magnetized Sphere Moving Slip Flow
- Materials Research Summary
- Measure Heat Transfer An Experimental
- Mixing Length Applicability
- Momentum Simultaneous Transfer
- Nonequilibrium Exact Solutions
- Nonisothermal Plasma Without Collisions Magnetohydrodynamics
- Nonstationary The
- Number Some Reynolds
- On
- Oscillation The
- Partially Ionized Hydrogen The Equation
- Plane Dissociation Relaxation
- Plasma Excitation
- Polyatomic Gas Heat Conduction
- Preliminary Description
- Pressure
- Radiant Heat Aerodynamic
- Reattachment Heat Transfer
- Recombination The Effect
- Research Objectives Dyna Soar
- Research Program The
- Sandia High-Altitude Sampler Design
- Shock Tube Plasma Studies
- Shock Tunnel Development Summary
- Shock Tunnel Development Summary
- Shock-Layer Hypersonic
- Similar On
- Stagnation-Point A Comparison
- Stagnation-Point Boundary The
- Structure Shock Layer
- Supersonic Flow Effect
- Supersonic Shear Flow Boundary Layer
- Surface Preparation Effect
- Table Compressible Flow
- Temperature Recovery
- Tensor Some Effects
- Thermodynamic Conditions Behind Reflected Hydrodynamic
- Thermodynamic Functions Ideal Gas
- Thermodynamic Tables
- Transfer Between Nongray Parallel Radiant Heat
- Transition Layer Structure
- Turbulent On
- Unit Reynolds Number Effects
- Wings Recent Hypersonic
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Bibliography
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- Adamson D. S.
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- Hannan E. J.
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- Hartley D. S.
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- Hillerman H. H.
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- Hoaglin D. C.
- Honig J.
- Hood J. W.
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- Hopgood R. E.
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- Hugus D. K.
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- Kahan J. H.
- Karr A. R
- Karr A. R
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- Kelleher G. J.
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- Kline M.
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- Koopmans T. C.
- Lanchester R W
- Larson H. J.
- Leake L. A.
- Linstone H. A.
- Livingston L
- Low L. J.
- Mailart J. D.
- March J. G.
- Massey H. G.
- Mathematical Formulations
- Mathematical Tables
- Mobile Missile Survival Against
- Model Documentation
- Mood A. M.
- Moroney M. J.
- Neter
- Novick D.
- Paulson R. M.
- Phelps M. W.
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- Roebuck J.
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- Staff Officer's Field Manual
- Steneck N. H.
- System
- System Simulator Capabilities Description
- Tank
- The Rand Corporation
- Theil H.
- Thomas
- Tiede R. V
- Tinall J. B.
- Tippett
- Tukey J.W.
- Wadsworth G. P.
- Wald A.
- Walker G. A.
- Walker L. K.
- Wallis W. A.
- Walther H. J.
- Watson G. S.
- Weaver W.
- Wetzler E.
- White W
- Willard D.
- Williamson O. E.
- Wilson A.
- Yergin D.
- Zellner A.
- Zimmerman R. E.
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study