Results 241 to 250 of about 151,552 (312)

Geometrically nonlinear high-fidelity aerostructural optimization for highly flexible wings. [PDF]

Struct Multidiscipl Optim
Gray AC, Kennedy GJ, Martins JRRA.
europepmc   +1 more source

Contact area and tissue growth dynamics shape synthetic juxtacrine signaling patterns. [PDF]

Biophys J
Dawson JE, Bryant A, Walton B, Bhikot S, Macon S, Ajamu-Johnson A, Jordan T, Langridge PD, Malmi-Kakkada AN.   +8 more
europepmc   +1 more source

Nitrogen Isotopes Suggest Sex-Based Diet Differences on the Breeding Grounds for a Sexually Monomorphic Migratory Passerine. [PDF]

Ecol Evol
Iverson AR, Cormier RL, Humple DL, Hahn TP, Schaefer J, Hull EM, Sakai WH, Simard-Provençal S.   +7 more
europepmc   +1 more source

Another tail of two sites: activation of the Notch ligand Delta by Mindbomb1. [PDF]

BMC Biol
Vüllings N, Airich A, Seib E, Troost T, Klein T.   +4 more
europepmc   +1 more source

Field Evaluation of Synthetic Components of the Sex Pheromone of the Tea Pest <i>Helopeltis cinchonae</i> Mann (Hemiptera: Miridae). [PDF]

Insects
Magsi FH, Hall DR, Luo Z, Meng X, Xiu C, Li Z, Bian L, Fu N, Li J, Chen Z, Cai X.   +10 more
europepmc   +1 more source

Comprehensive Engineering Performance Evaluation of the IRRAflow Active Fluid Exchange System with IRRAS Bolt for Intracranial Fluid Management. [PDF]

Cureus
Rezai Jahromi B, Badr R, Asbury D, Unser J.   +3 more
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Manufacturing and Preliminary Testing of Nano-Filled Elastomeric Film Cover for Morphing Airfoil. [PDF]

Sensors (Basel)
Ciminello M, Piscitelli F, Volponi R, Ameduri S.   +3 more
europepmc   +1 more source

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Buffeting Flows over Delta Wings

AIAA Journal, 1999
Experimental evidence suggests that vortex breakdown is not the only source of buffeting of delta wings and fins. Other unsteady flow phenomena that contribute to buffeting at high angles of attack are fluctuations of vortex breakdown location and vortex shedding.
Ismet Gursul, Wensheng Xie
openaire   +1 more source

Subsonic wing rock of slender delta wings

Journal of Aircraft, 1985
Two recent experimental studies investigated the s elf-excited motion Of a flat deita wing that was free to roll about an axis parallel to its mid-span chord. In this paper these experiments are s imulated numerically. An unsteady vortex-lattice method is used to provide the aerodynamic loads, and the equation of motion is integrated by a prediction ...
P. KONSTADINOPOULOS, D. MOOK, A. NAYFEH
openaire   +1 more source