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2015 IEEE Aerospace Conference : 7-14 March 2015
| 2015 IEEE Aerospace Conference : 7-14 March 2015 |
| Pubbl/distr/stampa | New York : , : IEEE, , 2015 |
| Descrizione fisica | 1 online resource (437 pages) |
| Soggetto topico |
Planets - Exploration
Artificial satellites Space vehicles |
| ISBN | 1-4799-5380-6 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910131257603321 |
| New York : , : IEEE, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
2015 IEEE Aerospace Conference : 7-14 March 2015
| 2015 IEEE Aerospace Conference : 7-14 March 2015 |
| Pubbl/distr/stampa | New York : , : IEEE, , 2015 |
| Descrizione fisica | 1 online resource (437 pages) |
| Soggetto topico |
Planets - Exploration
Artificial satellites Space vehicles |
| ISBN | 1-4799-5380-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISA-996280836003316 |
| New York : , : IEEE, , 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
| ||
AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others]
| AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
| Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
| Descrizione fisica | 1 online resource (525 p.) |
| Disciplina | 629.1323 |
| Collana | Applied mechanics and materials |
| Soggetto topico | Space vehicles |
| Soggetto genere / forma | Electronic books. |
| ISBN | 3-03826-616-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; Chapter 1: Aerodynamics; Numerical Simulation of Noise Radiated from a Blunt Trailing Edge; Further Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic Principles; Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles; Visualization of Flow Field and Wake over Clean and Under-Loaded Wings; NACA 4415 Wing Modification Using Tubercles - A Numerical Analysis
Comparison of Digital DATCOM and Wind Tunnel Data of a Winged Hybrid Airship's Generic ModelAn Experimental and Computational Fluid Dynamic Study of Axis-Symmetric Coanda Configuration for VTOL MAV Applications; Sensing Unsteady Pressure on MAV Wings: A New Method for Turbulence Alleviation; Chapter 2: Aerospace Structure; Multiple Crack Interactions in Bi-Material Plates under Mode I Tension Loading; Finite Element Computational Modeling and Simulation Studies of Non-Penetrating Impact Using Fundamental Principles; LCO Flutter Analysis on Coir Pressed Mat Fibre/Epoxy Composites Plate Quasi Static Analysis of a Biocomposite Aircraft RadomeModal Analysis of Thin Walled Multi-Cell Multi-Tapered Composite Beams of Closed Cross Sections; On the Dynamic Model of a Functionally Graded Spinning Structural Element of an Aircraft Appendage; Chapter 3: Propulsion; A Computational and Analytical Study into the Use of Counter-Flow Fluidic Thrust Vectoring Nozzle for Small Gas Turbine Engines; Computational Exploration of a Two-Spool High Bypass Turbofan Engine's Component Deterioration Effects on Engine Performance; CFD Validation and Analysis of a Single-Stage Axial Compressor Aerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine CascadeSpray Characteristics of an Internal-Mix Airblast Atomizer; Computational Approach in Sizing of Pulsejet Engine; Chapter 4: Aerospace Design; Application of Coandă Jet for Generating Lift of Micro Air Vehicles - Preliminary Design Considerations; Performance Calculations within the Conceptual Design Process of Hand-Launched Aircraft; Conceptual Design of Flapping Wing Using Shape Memory Alloy Actuator for Micro Unmanned Aerial Vehicle Design and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element ApproachReverse Engineering of a Fixed Wing Unmanned Aircraft 6-DoF Model for Navigation and Guidance Applications; Development of Blimp Platform for Aerial Photography; Autonomous Aerial Hard Docking of Fixed and Rotary Wing UAVs: Task Assessment and Solution Architecture; Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation; Chapter 5: Aerospace System Performance; The Application of Multiple Vibration Neutralizers for Vibration Control in Aircraft Effects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances |
| Record Nr. | UNINA-9910459893603321 |
| Switzerland : , : TTP, , [2014] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others]
| AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
| Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
| Descrizione fisica | 1 online resource (525 p.) |
| Disciplina | 629.1323 |
| Collana | Applied mechanics and materials |
| Soggetto topico | Space vehicles |
| ISBN | 3-03826-616-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; Chapter 1: Aerodynamics; Numerical Simulation of Noise Radiated from a Blunt Trailing Edge; Further Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic Principles; Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles; Visualization of Flow Field and Wake over Clean and Under-Loaded Wings; NACA 4415 Wing Modification Using Tubercles - A Numerical Analysis
Comparison of Digital DATCOM and Wind Tunnel Data of a Winged Hybrid Airship's Generic ModelAn Experimental and Computational Fluid Dynamic Study of Axis-Symmetric Coanda Configuration for VTOL MAV Applications; Sensing Unsteady Pressure on MAV Wings: A New Method for Turbulence Alleviation; Chapter 2: Aerospace Structure; Multiple Crack Interactions in Bi-Material Plates under Mode I Tension Loading; Finite Element Computational Modeling and Simulation Studies of Non-Penetrating Impact Using Fundamental Principles; LCO Flutter Analysis on Coir Pressed Mat Fibre/Epoxy Composites Plate Quasi Static Analysis of a Biocomposite Aircraft RadomeModal Analysis of Thin Walled Multi-Cell Multi-Tapered Composite Beams of Closed Cross Sections; On the Dynamic Model of a Functionally Graded Spinning Structural Element of an Aircraft Appendage; Chapter 3: Propulsion; A Computational and Analytical Study into the Use of Counter-Flow Fluidic Thrust Vectoring Nozzle for Small Gas Turbine Engines; Computational Exploration of a Two-Spool High Bypass Turbofan Engine's Component Deterioration Effects on Engine Performance; CFD Validation and Analysis of a Single-Stage Axial Compressor Aerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine CascadeSpray Characteristics of an Internal-Mix Airblast Atomizer; Computational Approach in Sizing of Pulsejet Engine; Chapter 4: Aerospace Design; Application of Coandă Jet for Generating Lift of Micro Air Vehicles - Preliminary Design Considerations; Performance Calculations within the Conceptual Design Process of Hand-Launched Aircraft; Conceptual Design of Flapping Wing Using Shape Memory Alloy Actuator for Micro Unmanned Aerial Vehicle Design and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element ApproachReverse Engineering of a Fixed Wing Unmanned Aircraft 6-DoF Model for Navigation and Guidance Applications; Development of Blimp Platform for Aerial Photography; Autonomous Aerial Hard Docking of Fixed and Rotary Wing UAVs: Task Assessment and Solution Architecture; Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation; Chapter 5: Aerospace System Performance; The Application of Multiple Vibration Neutralizers for Vibration Control in Aircraft Effects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances |
| Record Nr. | UNINA-9910787244503321 |
| Switzerland : , : TTP, , [2014] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others]
| AEROTECH V : progressive aerospace research : selected, peer reviewed papers from the AEROTECH V Conference, October 29-30, 2014, Kuala Lumpur, Malaysia / / edited by R. Varatharajoo [and four others] |
| Pubbl/distr/stampa | Switzerland : , : TTP, , [2014] |
| Descrizione fisica | 1 online resource (525 p.) |
| Disciplina | 629.1323 |
| Collana | Applied mechanics and materials |
| Soggetto topico | Space vehicles |
| ISBN | 3-03826-616-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTECH V: Progressive Aerospace Research; Preface and Editorial Panel; Table of Contents; Chapter 1: Aerodynamics; Numerical Simulation of Noise Radiated from a Blunt Trailing Edge; Further Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic Principles; Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles; Visualization of Flow Field and Wake over Clean and Under-Loaded Wings; NACA 4415 Wing Modification Using Tubercles - A Numerical Analysis
Comparison of Digital DATCOM and Wind Tunnel Data of a Winged Hybrid Airship's Generic ModelAn Experimental and Computational Fluid Dynamic Study of Axis-Symmetric Coanda Configuration for VTOL MAV Applications; Sensing Unsteady Pressure on MAV Wings: A New Method for Turbulence Alleviation; Chapter 2: Aerospace Structure; Multiple Crack Interactions in Bi-Material Plates under Mode I Tension Loading; Finite Element Computational Modeling and Simulation Studies of Non-Penetrating Impact Using Fundamental Principles; LCO Flutter Analysis on Coir Pressed Mat Fibre/Epoxy Composites Plate Quasi Static Analysis of a Biocomposite Aircraft RadomeModal Analysis of Thin Walled Multi-Cell Multi-Tapered Composite Beams of Closed Cross Sections; On the Dynamic Model of a Functionally Graded Spinning Structural Element of an Aircraft Appendage; Chapter 3: Propulsion; A Computational and Analytical Study into the Use of Counter-Flow Fluidic Thrust Vectoring Nozzle for Small Gas Turbine Engines; Computational Exploration of a Two-Spool High Bypass Turbofan Engine's Component Deterioration Effects on Engine Performance; CFD Validation and Analysis of a Single-Stage Axial Compressor Aerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine CascadeSpray Characteristics of an Internal-Mix Airblast Atomizer; Computational Approach in Sizing of Pulsejet Engine; Chapter 4: Aerospace Design; Application of Coandă Jet for Generating Lift of Micro Air Vehicles - Preliminary Design Considerations; Performance Calculations within the Conceptual Design Process of Hand-Launched Aircraft; Conceptual Design of Flapping Wing Using Shape Memory Alloy Actuator for Micro Unmanned Aerial Vehicle Design and Analysis of an Aircraft Composite Hinge Bracket Using Finite Element ApproachReverse Engineering of a Fixed Wing Unmanned Aircraft 6-DoF Model for Navigation and Guidance Applications; Development of Blimp Platform for Aerial Photography; Autonomous Aerial Hard Docking of Fixed and Rotary Wing UAVs: Task Assessment and Solution Architecture; Aeroelastic Tailoring of Composite Wing Design Using Bee Colony Optimisation; Chapter 5: Aerospace System Performance; The Application of Multiple Vibration Neutralizers for Vibration Control in Aircraft Effects of Aircraft Tail Configurations on Sensitivity to Yaw Disturbances |
| Record Nr. | UNINA-9910823858303321 |
| Switzerland : , : TTP, , [2014] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Apollo experience report : flight instrumentation calibration / / by J.F. DeMoss
| Apollo experience report : flight instrumentation calibration / / by J.F. DeMoss |
| Autore | DeMoss J. F. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1973 |
| Descrizione fisica | 1 online resource (11 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Astronautical instruments - Calibration Space vehicles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Apollo experience report |
| Record Nr. | UNINA-9910716562403321 |
DeMoss J. F.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Astrodynamics
| Astrodynamics |
| Pubbl/distr/stampa | [Beijing] : , : Tsinghua University Press |
| Descrizione fisica | 1 online resource |
| Soggetto topico |
Astrodynamics
Aerospace engineering Astronautics Space flight Space vehicles |
| Soggetto genere / forma | Periodicals. |
| Soggetto non controllato | Aeronautics Engineering & Astronautics |
| ISSN | 2522-0098 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910482000403321 |
| [Beijing] : , : Tsinghua University Press | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Centaur launch vehicle propellant utilization system / / by Steven V. Szabo, Jr., James A. Berns, Andrew J. Stofan
| Centaur launch vehicle propellant utilization system / / by Steven V. Szabo, Jr., James A. Berns, Andrew J. Stofan |
| Autore | Szabo Steven V., Jr. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (iii, 32 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Space vehicles
Propellants |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714070203321 |
|
Szabo Steven V., Jr.
|
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Challenge to Apollo : the Soviet Union and the Space Race, 1945-1974 / / by Asif A. Siddiqi
| Challenge to Apollo : the Soviet Union and the Space Race, 1945-1974 / / by Asif A. Siddiqi |
| Autore | Siddiqi Asif A. <1966-> |
| Pubbl/distr/stampa | Washington, DC : , : National Aeronautics and Space Administration, NASA History Division, Office of Policy and Plans, , 2000 |
| Descrizione fisica | 2 volumes (xvi-1011 pages) : illustrations |
| Collana | NASA/SP |
| Soggetto topico |
Space race
Space vehicles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Vol. I. Challenge to Apollo -- Vol. 2. Challenge to Apollo |
| Altri titoli varianti | Challenge to Apollo |
| Record Nr. | UNINA-9910716555303321 |
|
Siddiqi Asif A. <1966->
|
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| Washington, DC : , : National Aeronautics and Space Administration, NASA History Division, Office of Policy and Plans, , 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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China's advanced weapons systems / / lead author, Tate Nurkin, contributing authors, Kelly Bedard, James Clad, Cameron Scott, Jon Grevatt
| China's advanced weapons systems / / lead author, Tate Nurkin, contributing authors, Kelly Bedard, James Clad, Cameron Scott, Jon Grevatt |
| Autore | Nurkin Tate |
| Pubbl/distr/stampa | [London, England] : , : Jane's by IHS Markit, , 2018 |
| Descrizione fisica | 1 online resource (250 pages) : illustrations, maps, color photographs |
| Soggetto topico |
Military research - China
Military robots - China Artificial intelligence - Military applications Military weapons - Technological innovations - China Directed-energy weapons Space vehicles Defense industries - China Space weapons Astronautics, Military - China Armed Forces - Weapons systems Astronautics, Military Defense industries Military policy Military research Military robots Military weapons - Technological innovations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715920103321 |
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Nurkin Tate
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| [London, England] : , : Jane's by IHS Markit, , 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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