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Split-flap display
Known as:
Flip-Display
, Solari departure board
, Solari
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A split-flap display, or sometimes simply flap display, is an electromechanical display device that presents changeable alphanumeric text, and…
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Related topics
Related topics
12 relations
Destination sign
Display device
Electronic visual display
Flight information display system
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Papers overview
Semantic Scholar uses AI to extract papers important to this topic.
2016
2016
Predictive model on the effect of restrictor on transfer function parameters on pneumatic control system
C. Ukpaka
2016
Corpus ID: 53391406
Mathematical model was developed to monitor and predict the influence of restrictor or the characteristics of the functional…
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2016
2016
Mars Sphere of Influence Maneuvers for NASA’s Evolvable Mars Campaign
R. Merrill
,
D. Komar
,
M. Qu
,
P. Chai
2016
Corpus ID: 114859304
NASA's Human Spaceflight Architecture Team is refining human exploration architectures that will extend human presence to the…
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2013
2013
Fabrication and Analysis of Small Flapping Wings
Jason Rue
,
Kelvin Chang
,
+6 authors
A. Chaudhuri
2013
Corpus ID: 116799637
Flapping winged micro air vehicles (MAVs) have been of interest due to their unique flying characteristics. Wing design is an…
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2012
2012
Aeroacoustic Study of a High-Fidelity Aircraft Model: Part 1- Steady Aerodynamic Measurements
M. Khorrami
,
Judith A. Hannon
,
D. Neuhart
,
Gregory A. Markowski
,
T. VandeVen
2012
Corpus ID: 51994797
In this paper, we present steady aerodynamic measurements for an 18% scale model of a Gulfstream air-craft. The high fidelity and…
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2009
2009
Optimization of crop canopy sensor placement for measuring nitrogen status in corn.
D. Roberts
,
V. Adamchuk
,
J. Shanahan
,
R. Ferguson
,
J. Schepers
2009
Corpus ID: 17274189
Active canopy sensors can be used to assess corn (Zea mays L.) N status and direct spatially-variable in-season N application…
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2004
2004
Computational Investigation of Airfoils with Miniature Trailing Edge Control Surfaces
Hak-Tae Lee
,
I. Kroo
2004
Corpus ID: 6340685
Miniature trailing edge effectors (MiTEs) are small flaps (typically 1% to 5% chord) actuated with deflection angles up to 90…
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Highly Cited
2002
Highly Cited
2002
Flutter Suppression for High Aspect Ratio Flexible Wings Using Microflaps
Hak-Tae Lee
,
I. Kroo
,
Stefan R. Bieniawski
2002
Corpus ID: 477765
Miniature trailing edge effectors (MiTEs) are small flaps (typically 1% to 5% chord) actuated with deflection angles up to 90…
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1999
1999
Criterios básicos para una política de prevención y control de drogas en Chile
G. Sunkel
,
Martín Hopenhayn
,
Ibán de Rementería
1999
Corpus ID: 161748876
Resumen En el Chile actual el problema de las drogas no solo se reconoce y se enfrenta, sino tambien se politiza y polemiza…
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1998
1998
Analysis and testing of a Mach-scaled helicopter rotor in hover with piezoelectric bender-actuated trailing-edge flaps
N. Koratkar
,
I. Chopra
Smart Structures
1998
Corpus ID: 108938689
This paper presents an analytic model and validation tests of Froude and Mach scaled rotors featuring piezoelectric bender…
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1996
1996
Design and testing of a helicopter trailing edge flap with piezoelectric stack actuators
Burtis T. Spencer
,
I. Chopra
Smart Structures and Materials + Nondestructive…
1996
Corpus ID: 111086100
This paper presents the results of research in using piezoelectric stacks to power a trailing edge flap for use as an individual…
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