Explore: Aerodynamic Stalling
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Source: The Open Library
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Search results from The Open Library
1Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:
- Title: ➤ 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- Author: R. A. Piziali
- Language: English
- Number of Pages: Median: 559
- Publisher: ➤ National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic coefficients - Pressure distribution - Wind tunnel tests - Wind oscillations - Angle of attack - Airfoils - Aerodynamic stalling - Semispan models - Stalling - Oscillating wing aerodynamics
Edition Identifiers:
- The Open Library ID: OL17007551M - OL15409387M - OL18079048M - OL19754822M - OL17114716M
- Online Computer Library Center (OCLC) ID: 32770651
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight
By G. H. Gaonkar
“Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight” Metadata:
- Title: ➤ Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight
- Author: G. H. Gaonkar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering
- Publish Date: 1986 - 1987
- Publish Location: ➤ Boca Raton, FL - Springfield, Va - [Washington, DC
“Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight” Subjects and Themes:
- Subjects: ➤ Rotor body interactions - Wind tunnel tests - Airplanes - Rotary stability - Design and construction - Hovering stability - Rigid rotors - Aerodynamic stalling
Edition Identifiers:
- The Open Library ID: OL15411276M - OL15400581M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Airfoil dynamic stall and rotorcraft maneuverability
By William G. Bousman
“Airfoil dynamic stall and rotorcraft maneuverability” Metadata:
- Title: ➤ Airfoil dynamic stall and rotorcraft maneuverability
- Author: William G. Bousman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2000
- Publish Location: ➤ Hanover, MD - Moffett Field, Calif
“Airfoil dynamic stall and rotorcraft maneuverability” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Maneuverability - Airfoil profiles - Vortices - Thrust - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL17718301M - OL17607321M
- Online Computer Library Center (OCLC) ID: 50820078
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Study of the unsteady flow features on a stalled wing
By S. Yon
“Study of the unsteady flow features on a stalled wing” Metadata:
- Title: ➤ Study of the unsteady flow features on a stalled wing
- Author: S. Yon
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Reston, VA - [Washington, DC
“Study of the unsteady flow features on a stalled wing” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Angle of attack - Flow distribution - Frequencies - Rectangular wings - Separated flow - Subsonic wind tunnels - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL15539182M - OL17838077M
- Online Computer Library Center (OCLC) ID: 40832683
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Evaluation of turbulence models for unsteady flows of an oscillating airfoil
By G. R. Srinivasan
“Evaluation of turbulence models for unsteady flows of an oscillating airfoil” Metadata:
- Title: ➤ Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Author: G. R. Srinivasan
- Language: English
- Publisher: ➤ Pergamon - National Technical Information Service, distributor] - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [New York] - [Washington, D.C - Springfield, Va
“Evaluation of turbulence models for unsteady flows of an oscillating airfoil” Subjects and Themes:
- Subjects: ➤ Aerodynamic stalling - Airfoils - Computational fluid dynamics - Finite difference theory - Flow distribution - Navier-Stokes equation - Oscillations - Separated flow - Turbulence models - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL15504033M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8An analysis of the crossover between local and massive separation on airfoils
By Mark Barnett
“An analysis of the crossover between local and massive separation on airfoils” Metadata:
- Title: ➤ An analysis of the crossover between local and massive separation on airfoils
- Author: Mark Barnett
- Number of Pages: Median: 103
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“An analysis of the crossover between local and massive separation on airfoils” Subjects and Themes:
- Subjects: Aerodynamic stalling - Airfoils - Separation - Viscous-inviscid interaction
Edition Identifiers:
- The Open Library ID: OL19249308M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Aerodynamic simulation of ice accretion on airfoils
By Andy P. Broeren
“Aerodynamic simulation of ice accretion on airfoils” Metadata:
- Title: ➤ Aerodynamic simulation of ice accretion on airfoils
- Author: Andy P. Broeren
- Language: English
- Number of Pages: Median: 66
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2011
- Publish Location: Cleveland, Ohio
“Aerodynamic simulation of ice accretion on airfoils” Subjects and Themes:
- Subjects: ➤ Airfoils - Ice formation - Wind tunnel tests - Aerodynamic stalling - Scale models - Simulation
Edition Identifiers:
- The Open Library ID: OL43888753M
- Online Computer Library Center (OCLC) ID: 769137623
Access and General Info:
- First Year Published: 2011
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Analysis of fully stalled compressor
By Wojciech Rostafiński
“Analysis of fully stalled compressor” Metadata:
- Title: ➤ Analysis of fully stalled compressor
- Author: Wojciech Rostafiński
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Analysis of fully stalled compressor” Subjects and Themes:
- Subjects: Aerodynamic stalling - Compressor rotors - Stalling (Aerodynamics) - Structural design criteria - Supersonic compressors
Edition Identifiers:
- The Open Library ID: OL16151249M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
By Edward C. Polhamus
“A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Metadata:
- Title: ➤ A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
- Author: Edward C. Polhamus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
- Publish Date: 1996
- Publish Location: Springfield, VA - Hampton, Va
“A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Subjects and Themes:
- Subjects: Aerodynamic stalling - Leading edges - Low speed - Swept wings - Wing planforms
Edition Identifiers:
- The Open Library ID: OL15490451M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Cellular structures in the flow over the flap of a two-element wing
By Steven A. Yon
“Cellular structures in the flow over the flap of a two-element wing” Metadata:
- Title: ➤ Cellular structures in the flow over the flap of a two-element wing
- Author: Steven A. Yon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Cellular structures in the flow over the flap of a two-element wing” Subjects and Themes:
- Subjects: ➤ Rectangular wings - Pressure ratio - Aerodynamic stalling - Time dependence - Flow visualization - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15504783M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight
By G. H. Gaonkar
“Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” Metadata:
- Title: ➤ Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight
- Author: G. H. Gaonkar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
- Publish Date: 1996
- Publish Location: ➤ Boca Raton, FL - Springfield, Va - [Washington, DC
“Predictions of control inputs, periodic responses and damping levels of an isolated experimental rotor in trimmed flight” Subjects and Themes:
- Subjects: ➤ Aerodynamic balance - Lateral control - Aerodynamic stalling - Aeroelasticity - Rotor aerodynamics - Flight tests - Airfoils
Edition Identifiers:
- The Open Library ID: OL17126375M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
By G. H. Gaonkar
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Metadata:
- Title: ➤ Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
- Author: G. H. Gaonkar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
- Publish Date: 1994
- Publish Location: ➤ Boca Raton, FL - Springfield, Va - [Washington, DC
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic drag - Wakes - Aerodynamic stalling - Torsional vibration - Aeroelasticity - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL17029328M
- Online Computer Library Center (OCLC) ID: 32035217
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations
By Koji Isogai
“Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations” Metadata:
- Title: ➤ Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations
- Author: Koji Isogai
- Number of Pages: Median: 23
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Tokyo
“Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations” Subjects and Themes:
- Subjects: Aerodynamic stalling - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19249026M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16The phenomenon of dynamic stall
By W. J. McCroskey
“The phenomenon of dynamic stall” Metadata:
- Title: ➤ The phenomenon of dynamic stall
- Author: W. J. McCroskey
- Publisher: Ames Research Center
- Publish Date: 1981
- Publish Location: Moffett Field, Calif
“The phenomenon of dynamic stall” Subjects and Themes:
- Subjects: Aerodynamic stalling
Edition Identifiers:
- The Open Library ID: OL20898737M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Some observations on transitory stall in conical diffusers
By K. B. M. Q. Zaman
“Some observations on transitory stall in conical diffusers” Metadata:
- Title: ➤ Some observations on transitory stall in conical diffusers
- Author: K. B. M. Q. Zaman
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“Some observations on transitory stall in conical diffusers” Subjects and Themes:
- Subjects: Aerodynamic stalling - Conical flow - Diffusion - Boundary layer separation - Pressure recovery
Edition Identifiers:
- The Open Library ID: OL16122156M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane
By H. Paul Stough
“Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane” Metadata:
- Title: ➤ Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane
- Author: H. Paul Stough
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane” Subjects and Themes:
- Subjects: ➤ Handling characteristics - Spin (Aerodynamics) - Aeronautics - Aircraft spin - Airplanes - Stalling (Aerodynamics) - Spin dynamics - Aerodynamic stalling - Angular momentum
Edition Identifiers:
- The Open Library ID: OL16115014M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
By Robert Alan Hess
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Metadata:
- Title: ➤ Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data
- Author: Robert Alan Hess
- Language: English
- Number of Pages: Median: 63
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data” Subjects and Themes:
- Subjects: ➤ Airplanes - Aerodynamics - Wing profiles - Aircraft stability - Aerodynamic stalling - Leading edges - General aviation aircraft - Wings - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL16152660M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
By R. H. Landon
“A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Metadata:
- Title: ➤ A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
- Author: R. H. Landon
- Publisher: ➤ Aircraft Research Association Ltd
- Publish Date: 1977
- Publish Location: Manton Lane, Bedford, England
“A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Subjects and Themes:
- Subjects: Aerodynamic loads - Aerodynamic stalling - Rotary wings - Helicopters
Edition Identifiers:
- The Open Library ID: OL20966945M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data
By C. M. Tan
“The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” Metadata:
- Title: ➤ The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data
- Author: C. M. Tan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data” Subjects and Themes:
- Subjects: ➤ Dynamic response - Helicopter design - Rectangular wings - Oscillating flow - Aerodynamic stalling - Unswept wings - Wing oscillations
Edition Identifiers:
- The Open Library ID: OL15498137M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Effect of acoustic excitation on stalled flows over an airfoil
By K. B. M. O. Zaman
“Effect of acoustic excitation on stalled flows over an airfoil” Metadata:
- Title: ➤ Effect of acoustic excitation on stalled flows over an airfoil
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Effect of acoustic excitation on stalled flows over an airfoil” Subjects and Themes:
- Subjects: Aerodynamic stalling - Acoustic excitation - Airfoil profiles - Boundary layer separation - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405867M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23A steadying effect of acoustic excitation on transitory stall
By K. B. M. O. Zaman
“A steadying effect of acoustic excitation on transitory stall” Metadata:
- Title: ➤ A steadying effect of acoustic excitation on transitory stall
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“A steadying effect of acoustic excitation on transitory stall” Subjects and Themes:
- Subjects: ➤ Separated flow - Airfoils - Aerodynamic stalling - Backward facing steps - Acoustic excitation - Diffusers - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405548M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A steadying effect of acoustic excitation on transitory stall at online marketplaces:
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- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
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Stall (fluid dynamics)
Stalling is caused by flow separation which, in turn, is caused by the air flowing against a rising pressure. Whitford describes three types of stall:
Vortex generator
contact with the airfoil surface, delays local flow separation and aerodynamic stalling, thereby improving the effectiveness of wings and control surfaces
Stick shaker
"stick") of an aircraft, warning the flight crew that an imminent aerodynamic stall has been detected. It is typically present on the majority of large
Colgan Air Flight 3407
Approaching Buffalo, the aircraft, a Bombardier Q400, entered an aerodynamic stall from which it did not recover and crashed into a house at 6038 Long
Stall strips
A stall strip is a small component fixed to the leading edge of the wing of an airplane to modify its aerodynamic characteristics. These stall strips may
USAir Flight 427
opposite to that commanded by the pilots, causing the plane to enter an aerodynamic stall from which Captain Peter Germano and First Officer Charles B. Emmet
Stick pusher
entering an aerodynamic stall. Some large fixed-wing aircraft display poor post-stall handling characteristics or are vulnerable to deep stall. To prevent
Lauda Air Flight 004
1 engine during the climb phase, causing the aircraft to enter an aerodynamic stall, uncontrolled dive, and in-flight breakup, killing all 213 passengers
Chandelle
heading at an airspeed in the "slow-flight" regime, very near the aerodynamic stall. The aircraft can be flown in "slow-flight" after establishing the
Air France Flight 447
miscommunication led to the pilots inadvertently stalling the Airbus A330. They failed to recover the aircraft from the stall, and the aircraft crashed into the mid-Atlantic