Effect Of Crosswinds On A Stol Aircraft During Landing
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A Flight Investigation Of Piloting Techniques And Crosswind Limitations During Visual Stol Type Landing Operations
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Author : Langley Research Center
language : en
Publisher:
Release Date : 1976
A Flight Investigation Of Piloting Techniques And Crosswind Limitations During Visual Stol Type Landing Operations written by Langley Research Center and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Airplanes categories.
Effect Of Crosswinds On A Stol Aircraft During Landing
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Author : Craig Ross Jones
language : en
Publisher:
Release Date : 1973
Effect Of Crosswinds On A Stol Aircraft During Landing written by Craig Ross Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
A Flight Examination Of Operating Problems Of V Stol Aircraft In Stol Type Landing And Approach
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Author : Robert C. Innis
language : en
Publisher:
Release Date : 1961
A Flight Examination Of Operating Problems Of V Stol Aircraft In Stol Type Landing And Approach written by Robert C. Innis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Astronautics categories.
Effect Of A 90 Cross Wind On The Take Off Distance Of A Light Airplane Equipped With A Cross Wind Landing Gear
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Author : Seth B. Anderson
language : en
Publisher:
Release Date : 1949
Effect Of A 90 Cross Wind On The Take Off Distance Of A Light Airplane Equipped With A Cross Wind Landing Gear written by Seth B. Anderson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Airplanes categories.
Flight tests were conducted with a light airplane equipped with a cross-wind landing gear to compare the ground distance required for take-off in calm air and with a 90 degree cross wind. These tests show that approximately 24 percent less ground run was required to attain take-off speeds of 40 to 50 miles per hour in a 16-mile-per-hour 90 degrees cross wind than in calm air.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1973
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aeronautics categories.
Nasa Technical Note
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1959
Nasa Technical Note written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aeronautics categories.
Flight Investigation Of Piloting Techniques And Crosswind Limitations Using A Research Type Crosswind Landing Gear
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Author :
language : en
Publisher:
Release Date : 1979
Flight Investigation Of Piloting Techniques And Crosswind Limitations Using A Research Type Crosswind Landing Gear written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.
A Flight Evaluation Of A Vtol Jet Transport Under Visual And Simulated Instrument Conditions
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Author : Curt A. Holzhauser
language : en
Publisher:
Release Date : 1972
A Flight Evaluation Of A Vtol Jet Transport Under Visual And Simulated Instrument Conditions written by Curt A. Holzhauser and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Aircraft categories.
A flight investigation was performed with the Dornier DO-31 VTOL to evaluate the performance, handling qualities, and operating characteristics that are considered to be important in the operation of a commercial VTOL transport in the terminal area. The DO-31, a 20,000 kilogram transport, has a mixed jet propulsion system; main engines with nozzles deflect from a cruise to a hover position, and vertical lift engines operated below 170 knots. This VTOL mode incorporates pitch and roll attitude and yaw rate stabilization. The tests concentrated on the transition, approach, and vertical landing. The mixed jet propulsion system provided a large usable performance envelope that enabled simulated IFR approaches to be made on 7 deg and 12 deg glide slopes. In these approaches management of thrust magnitude and direction was a primary problem, and some form of integrating the controls will be necessary. The handling qualities evaluation pointed out the need for additional research of define flight path criteria. The aircraft had satisfactory control and stability in hover out of ground effect. The recirculation effects in vertical landing were large below 15 meters.
Proceedings Of The 1985 Nasa Ames Research Center S Ground Effects Workshop
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Author : Kerry Mitchell
language : en
Publisher:
Release Date : 1987
Proceedings Of The 1985 Nasa Ames Research Center S Ground Effects Workshop written by Kerry Mitchell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Ground-cushion phenomenon categories.