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Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) / / R.M. Martin [and three others]
Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) / / R.M. Martin [and three others]
Autore Martin R. M (Ruth McVoy), <1956->
Pubbl/distr/stampa Washington, DC : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , 1988
Descrizione fisica 1 online resource (iii, 178 pages) : illustrations
Collana NASA technical memorandum
AVSCOM technical report
Soggetto topico Acoustic measurement
Blade-vortex interaction
Helicopters
Rotors
Wind tunnel models
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel
Record Nr. UNINA-9910704958803321
Martin R. M (Ruth McVoy), <1956->  
Washington, DC : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , 1988
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Modl/HIRES: methodology and users' manual / / D. Douglas Boyd, Jr. [and three others]
Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Modl/HIRES: methodology and users' manual / / D. Douglas Boyd, Jr. [and three others]
Autore Boyd D. Douglas
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 1998
Descrizione fisica 1 online resource (vii, 224 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aeroacoustics
Applications programs (computers)
Blade slap noise
Blade-vortex interaction
Helicopters
Noise prediction
Rotor aerodynamics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Modl/HIRES
Record Nr. UNINA-9910705875203321
Boyd D. Douglas  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham
Autore Noonan Kevin W.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Descrizione fisica 1 online resource (82 pages) : chiefly illustrations
Collana NASA technical paper
AVRADCOM technical report
Soggetto topico Aerodynamic characteristics
Airfoils
Helicopters
Reynolds number
Wind tunnel tests
Aerofoils - Testing
Helicopters - Aerodynamics
Rotors (Helicopters) - Testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707473303321
Noonan Kevin W.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
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An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation / / W. Keats Wilkie, K.C. Park
An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation / / W. Keats Wilkie, K.C. Park
Autore Wilkie W. Keats
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1996
Descrizione fisica 1 online resource (iv, 58 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Aeroelasticity
Helicopters
Fiber composites
Rotary wings
Unsteady aerodynamics
Differential equations
Galerkin method
Numerical integration
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707239903321
Wilkie W. Keats  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Afghan Special Mission Wing : DOD moving forward with $771.8 million purchase of aircraft that Afghans cannot operate or maintain
Afghan Special Mission Wing : DOD moving forward with $771.8 million purchase of aircraft that Afghans cannot operate or maintain
Pubbl/distr/stampa [Arlington, Va.] : , : Special Inspector General for Afghanistan Reconstruction, , 2013
Descrizione fisica 1 online resource (ii, 33 pages) : color illustrations
Collana SIGAR audit
Soggetto topico Defense contracts - United States - Auditing
Airplanes, Military
Helicopters
Drug traffic - Afghanistan - Prevention - Finance
Terrorism - Afghanistan - Prevention - Finance
Waste in government spending - United States
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Afghan Special Mission Wing
Record Nr. UNINA-9910704634803321
[Arlington, Va.] : , : Special Inspector General for Afghanistan Reconstruction, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Art of the helicopter [[electronic resource] /] / John Watkinson
Art of the helicopter [[electronic resource] /] / John Watkinson
Autore Watkinson John <1950->
Pubbl/distr/stampa Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Descrizione fisica 1 online resource (405 p.)
Disciplina 629.133352
Soggetto topico Helicopters
Helicopters - Aerodynamics
Helicopters - Control systems
Helicopters - Electric equipment
Soggetto genere / forma Electronic books.
ISBN 1-280-96648-3
9786610966486
0-08-047203-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto front cover; copyright; table of contents; front matter; Preface; Acknowledgements; body; 1 Introduction to rotorcraft; 1.1 Applications of the helicopter; 1.2 A short technical helicopter history; 1.3 Types of rotorcraft; 1.4 Rotor configurations; 1.5 The essential elements; 1.6 The airframe; 1.7 Engine and transmission; 1.8 The fuel system; 1.9 The landing gear; 1.10 Oleos and ground resonance; 1.11 The rotors; 1.12 The control system; 1.13 Electrical and hydraulic system; 1.14 Instruments and avionics; 2 Technical background; 2.1 Introduction to mechanics; 2.2 Mass and density
2.3 Force and acceleration2.4 Strength and rigidity; 2.5 Resultants and components offorces; 2.6 Moments and couples; 2.7 Work,energy,power and momentum; 2.8 Efficiency; 2.9 Gases and the atmosphere; 2.10 Sound; 2.11 The mechanics ofoscillation; 2.12 The mechanics ofrotation; 2.13 Sidebands; 2.14 Fourier analysis; 2.15 Centrifugal and Coriolis forces; 2.16 Rotating masses and precession; 2.17 The gyroscope; 2.18 Piezo-electric and laser gyroscopes; 2.19 Feedback; 3 Introduction to helicopter dynamics; 3.1 Creating and controlling lift; 3.2 The centre of pressure; 3.3 The coefficient of lift
3.4 Collective control3.5 In the hover; 3.6 Forces on the blades; 3.7 Rotor coning; 3.8 Torque and thrust in rotors; 3.9 The rotor as an actuator; 3.10 Blade element theory; 3.11 Disc loading; 3.12 Figure of merit; 3.13 Blade twist and taper; 3.14 Swirl; 3.15 Vertical autorotation; 3.16 Tip loss and the vortex ring; 3.17Ground effect; 3.18 Cyclic control; 3.19 Basic manoeuvres; 3.20 In translational flight; 3.21 Inflow and coning roll; 3.22 Rotor H-force; 3.23 Blade stall and compressibility; 3.24 The speed limit; 3.25 Harmonic blade motion; 3.26 Sources of vibration; 3.27 Vibration control
3.28 Harmonic pitch control3.29 Blade design; 4 Rotors in practice; 4.1 Introduction; 4.2 Why articulated rotors are used; 4.3 Axes galore; 4.4 Flapping; 4.5 Droop stops; 4.6Introduction to dragging; 4.7 Order of hinges; 4.8 Types of rotor head; 4.9 Zero-offset heads; 4.10 Dangers of zero-offset heads -negative g; 4.11 Rotor response; 4.12 Feathering; 4.13 Pitch control; 4.14 Cyclic trim; 4.15 Tilting heads; 4.16 Dragging dynamics; 4.17 Ground resonance; 4.18 Air resonance; 4.19 Dynamic rollover; 4.20 Some rotor head examples; 4.21 Blade construction; 4.22 Blade tracking; 4.23 Blade folding
5 The tail5.1 Introduction; 5.2 Balancing the torque; 5.3 The conventional tail rotor; 5.4 Tail rotor location; 5.5 Tail rotor performance; 5.6 The tail plane; 5.7 The stabilator; 5.8 Fins; 5.9 The tail boom; 5.10 The fenestron; 5.11 NOTAR; 5.12 Tail rotor failure; 6 Engines and transmissions; 6.1 Introduction; 6.2 Choice of engine; 6.3 A piston-engine installation; 6.4 A turbine installation; 6.5 Correlators and governors; 6.6 The gasoline engine; 6.7 The ignition system; 6.8 The starter; 6.9 The oil system; 6.10 The carburettor; 6.11 Fuel injection; 6.12 The turbocharger
6.13 Gasoline engine instruments
Record Nr. UNINA-9910457310403321
Watkinson John <1950->  
Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Art of the helicopter [[electronic resource] /] / John Watkinson
Art of the helicopter [[electronic resource] /] / John Watkinson
Autore Watkinson John <1950->
Pubbl/distr/stampa Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Descrizione fisica 1 online resource (405 p.)
Disciplina 629.133352
Soggetto topico Helicopters
Helicopters - Aerodynamics
Helicopters - Control systems
Helicopters - Electric equipment
ISBN 1-280-96648-3
9786610966486
0-08-047203-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto front cover; copyright; table of contents; front matter; Preface; Acknowledgements; body; 1 Introduction to rotorcraft; 1.1 Applications of the helicopter; 1.2 A short technical helicopter history; 1.3 Types of rotorcraft; 1.4 Rotor configurations; 1.5 The essential elements; 1.6 The airframe; 1.7 Engine and transmission; 1.8 The fuel system; 1.9 The landing gear; 1.10 Oleos and ground resonance; 1.11 The rotors; 1.12 The control system; 1.13 Electrical and hydraulic system; 1.14 Instruments and avionics; 2 Technical background; 2.1 Introduction to mechanics; 2.2 Mass and density
2.3 Force and acceleration2.4 Strength and rigidity; 2.5 Resultants and components offorces; 2.6 Moments and couples; 2.7 Work,energy,power and momentum; 2.8 Efficiency; 2.9 Gases and the atmosphere; 2.10 Sound; 2.11 The mechanics ofoscillation; 2.12 The mechanics ofrotation; 2.13 Sidebands; 2.14 Fourier analysis; 2.15 Centrifugal and Coriolis forces; 2.16 Rotating masses and precession; 2.17 The gyroscope; 2.18 Piezo-electric and laser gyroscopes; 2.19 Feedback; 3 Introduction to helicopter dynamics; 3.1 Creating and controlling lift; 3.2 The centre of pressure; 3.3 The coefficient of lift
3.4 Collective control3.5 In the hover; 3.6 Forces on the blades; 3.7 Rotor coning; 3.8 Torque and thrust in rotors; 3.9 The rotor as an actuator; 3.10 Blade element theory; 3.11 Disc loading; 3.12 Figure of merit; 3.13 Blade twist and taper; 3.14 Swirl; 3.15 Vertical autorotation; 3.16 Tip loss and the vortex ring; 3.17Ground effect; 3.18 Cyclic control; 3.19 Basic manoeuvres; 3.20 In translational flight; 3.21 Inflow and coning roll; 3.22 Rotor H-force; 3.23 Blade stall and compressibility; 3.24 The speed limit; 3.25 Harmonic blade motion; 3.26 Sources of vibration; 3.27 Vibration control
3.28 Harmonic pitch control3.29 Blade design; 4 Rotors in practice; 4.1 Introduction; 4.2 Why articulated rotors are used; 4.3 Axes galore; 4.4 Flapping; 4.5 Droop stops; 4.6Introduction to dragging; 4.7 Order of hinges; 4.8 Types of rotor head; 4.9 Zero-offset heads; 4.10 Dangers of zero-offset heads -negative g; 4.11 Rotor response; 4.12 Feathering; 4.13 Pitch control; 4.14 Cyclic trim; 4.15 Tilting heads; 4.16 Dragging dynamics; 4.17 Ground resonance; 4.18 Air resonance; 4.19 Dynamic rollover; 4.20 Some rotor head examples; 4.21 Blade construction; 4.22 Blade tracking; 4.23 Blade folding
5 The tail5.1 Introduction; 5.2 Balancing the torque; 5.3 The conventional tail rotor; 5.4 Tail rotor location; 5.5 Tail rotor performance; 5.6 The tail plane; 5.7 The stabilator; 5.8 Fins; 5.9 The tail boom; 5.10 The fenestron; 5.11 NOTAR; 5.12 Tail rotor failure; 6 Engines and transmissions; 6.1 Introduction; 6.2 Choice of engine; 6.3 A piston-engine installation; 6.4 A turbine installation; 6.5 Correlators and governors; 6.6 The gasoline engine; 6.7 The ignition system; 6.8 The starter; 6.9 The oil system; 6.10 The carburettor; 6.11 Fuel injection; 6.12 The turbocharger
6.13 Gasoline engine instruments
Record Nr. UNINA-9910784328803321
Watkinson John <1950->  
Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Art of the helicopter [[electronic resource] /] / John Watkinson
Art of the helicopter [[electronic resource] /] / John Watkinson
Autore Watkinson John <1950->
Pubbl/distr/stampa Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Descrizione fisica 1 online resource (405 p.)
Disciplina 629.133352
Soggetto topico Helicopters
Helicopters - Aerodynamics
Helicopters - Control systems
Helicopters - Electric equipment
ISBN 1-280-96648-3
9786610966486
0-08-047203-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto front cover; copyright; table of contents; front matter; Preface; Acknowledgements; body; 1 Introduction to rotorcraft; 1.1 Applications of the helicopter; 1.2 A short technical helicopter history; 1.3 Types of rotorcraft; 1.4 Rotor configurations; 1.5 The essential elements; 1.6 The airframe; 1.7 Engine and transmission; 1.8 The fuel system; 1.9 The landing gear; 1.10 Oleos and ground resonance; 1.11 The rotors; 1.12 The control system; 1.13 Electrical and hydraulic system; 1.14 Instruments and avionics; 2 Technical background; 2.1 Introduction to mechanics; 2.2 Mass and density
2.3 Force and acceleration2.4 Strength and rigidity; 2.5 Resultants and components offorces; 2.6 Moments and couples; 2.7 Work,energy,power and momentum; 2.8 Efficiency; 2.9 Gases and the atmosphere; 2.10 Sound; 2.11 The mechanics ofoscillation; 2.12 The mechanics ofrotation; 2.13 Sidebands; 2.14 Fourier analysis; 2.15 Centrifugal and Coriolis forces; 2.16 Rotating masses and precession; 2.17 The gyroscope; 2.18 Piezo-electric and laser gyroscopes; 2.19 Feedback; 3 Introduction to helicopter dynamics; 3.1 Creating and controlling lift; 3.2 The centre of pressure; 3.3 The coefficient of lift
3.4 Collective control3.5 In the hover; 3.6 Forces on the blades; 3.7 Rotor coning; 3.8 Torque and thrust in rotors; 3.9 The rotor as an actuator; 3.10 Blade element theory; 3.11 Disc loading; 3.12 Figure of merit; 3.13 Blade twist and taper; 3.14 Swirl; 3.15 Vertical autorotation; 3.16 Tip loss and the vortex ring; 3.17Ground effect; 3.18 Cyclic control; 3.19 Basic manoeuvres; 3.20 In translational flight; 3.21 Inflow and coning roll; 3.22 Rotor H-force; 3.23 Blade stall and compressibility; 3.24 The speed limit; 3.25 Harmonic blade motion; 3.26 Sources of vibration; 3.27 Vibration control
3.28 Harmonic pitch control3.29 Blade design; 4 Rotors in practice; 4.1 Introduction; 4.2 Why articulated rotors are used; 4.3 Axes galore; 4.4 Flapping; 4.5 Droop stops; 4.6Introduction to dragging; 4.7 Order of hinges; 4.8 Types of rotor head; 4.9 Zero-offset heads; 4.10 Dangers of zero-offset heads -negative g; 4.11 Rotor response; 4.12 Feathering; 4.13 Pitch control; 4.14 Cyclic trim; 4.15 Tilting heads; 4.16 Dragging dynamics; 4.17 Ground resonance; 4.18 Air resonance; 4.19 Dynamic rollover; 4.20 Some rotor head examples; 4.21 Blade construction; 4.22 Blade tracking; 4.23 Blade folding
5 The tail5.1 Introduction; 5.2 Balancing the torque; 5.3 The conventional tail rotor; 5.4 Tail rotor location; 5.5 Tail rotor performance; 5.6 The tail plane; 5.7 The stabilator; 5.8 Fins; 5.9 The tail boom; 5.10 The fenestron; 5.11 NOTAR; 5.12 Tail rotor failure; 6 Engines and transmissions; 6.1 Introduction; 6.2 Choice of engine; 6.3 A piston-engine installation; 6.4 A turbine installation; 6.5 Correlators and governors; 6.6 The gasoline engine; 6.7 The ignition system; 6.8 The starter; 6.9 The oil system; 6.10 The carburettor; 6.11 Fuel injection; 6.12 The turbocharger
6.13 Gasoline engine instruments
Record Nr. UNINA-9910811288803321
Watkinson John <1950->  
Oxford ; ; Burlington, MA, : Elsevier Butterworth-Heinemann, 2004
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Art of the helicopter [e-book] / John Watkinson
Art of the helicopter [e-book] / John Watkinson
Autore Watkinson, John, 1950-
Pubbl/distr/stampa Oxford : Burlington, MA : Elsevier Butterworth-Heinemann, 2004
Descrizione fisica xii, 390 p. : ill. ; 26 cm.
Disciplina 629.133352
Soggetto topico Helicopters
Helicopters - Aerodynamics
Helicopters - Control systems
Helicopters - Electric equipment
Soggetto genere / forma Electronic books.
ISBN 9780750657150
0750657154
Formato Risorse elettroniche
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Chapter 1. Introduction to Rotorcraft -- Chapter 2. Technical Background -- Chapter 3. Introduction to Helicopter Dynamics -- Chapter 4. Rotors in Practice -- Chapter 5. The Tail -- Chapter 6. Engines and transmissions -- Chapter 7. Other types of rotorcraft -- Chapter 8. Flight Instruments -- Chapter 9. Control and stability -- Chapter 10. Helicopter Performance -- Chapter 11. Flying Training -- Index.
Record Nr. UNISALENTO-991003237879707536
Watkinson, John, 1950-  
Oxford : Burlington, MA : Elsevier Butterworth-Heinemann, 2004
Risorse elettroniche
Lo trovi qui: Univ. del Salento
Opac: Controlla la disponibilità qui
Characterization and comparison of vibration transfer paths in a helicopter gearbox and a fixture mounted gearbox / / Anwarul Islam [and three others]
Characterization and comparison of vibration transfer paths in a helicopter gearbox and a fixture mounted gearbox / / Anwarul Islam [and three others]
Autore Isalāma Ānoẏārula
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013
Descrizione fisica 1 online resource (21 pages) : color illustrations
Collana NASA/TM
Soggetto topico Systems health monitoring
Transmissions (machine elements)
Maintenance
Helicopters
Torque
Rotary wing aircraft
Alignment
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702656203321
Isalāma Ānoẏārula  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui