Skip to search form
Skip to main content
Skip to account menu
Semantic Scholar
Semantic Scholar's Logo
Search 238,227,574 papers from all fields of science
Search
Sign In
Create Free Account
cell trailing edge
Known as:
back of cell
, trailing edge
The area of a motile cell opposite to the direction of movement. [GOC:pg]
National Institutes of Health
Create Alert
Alert
Related topics
Related topics
2 relations
Narrower (2)
cell trailing edge membrane
uropod
Papers overview
Semantic Scholar uses AI to extract papers important to this topic.
Review
2012
Review
2012
NUMERICAL SIMULATION AND ANALYSIS OF COANDA EFFECT CIRCULATION CONTROL FOR WIND-TURBINE APPLICATION CONSIDERATIONS
D. H
,
Jojodihardjo
,
+6 authors
Ajid
2012
Corpus ID: 67781750
In the efforts to investigate the performance of Coanda Jet in enhancing lift of an airfoil, a numerical study is carried out…
Expand
2011
2011
Experimental characterization of airfoil boundary layers for improvement of aeroacoustic and aerodynamic modeling
A. Fischer
2011
Corpus ID: 125158325
and aerodynamic modeling DTU Orbit (03/11/2019) Experimental characterization of airfoil boundary layers for improvement of…
Expand
2008
2008
Real Airfoil Effects on Leading Edge Noise
Joshua Staubs
2008
Corpus ID: 125993265
2006
2006
Direct Noise Computation around a 3-D NACA 0012 airfoil
O. Marsden
,
C. Bogey
,
C. Bailly
2006
Corpus ID: 67756651
A Large Eddy Simulation of the flow around a NACA 0012 airfoil at a Reynolds number of 500,000 is presented. At this Reynolds…
Expand
2005
2005
The SHARCS project: Smart hybrid active rotor control system for noise and vibration attenuation of helicopter rotor blades
F. Nitzsche
,
D. Feszty
,
+5 authors
G. Ghiringhelli
2005
Corpus ID: 17737189
The SHARCS project aims to develop an actively controlled helicopter rotor for the simultaneous suppression of vibration and…
Expand
2003
2003
Flapping Motion of a Three-Dimensional Foil for Propulsion and Maneuvering of Underwater Vehicles
Melissa Flores
2003
Corpus ID: 108613353
Experiments were performed on a three-dimensional NACA 0015 foil with a 5.5 cm average chord and 24.3 cm span performing a…
Expand
Review
2002
Review
2002
Active Control of Flow Separation from the Slat Shoulder of a Supercritical Airfoil
L. Pack
,
N. Schaeffler
,
C. Yao
,
A. Seifert
2002
Corpus ID: 14779308
Active flow control in the form of periodic zero-mass-flux excitation was applied at the slat shoulder of a simplified high-lift…
Expand
1998
1998
Turbofan rotor/stator interaction noise reduction through trailing edge blowing
J. Brookfield
1998
Corpus ID: 111160347
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.
1997
1997
A comprehensive aeroelastic analysis of helicopter main rotors with trailing edge flaps for vibration reduction
J. Milgram
1997
Corpus ID: 109129241
1992
1992
A study of streamwise vortex enhanced mixing in lobed mixer devices
Jing-Qiu Yuan
1992
Corpus ID: 109447642
The effect of shed streamwise vorticity on mixing in a lobed mixer device has been examined computationally and experimentally…
Expand