Results 91 to 100 of about 150,010 (213)

The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear [PDF]

open access: yes
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7 by 10 foot wind tunnel. The flaps were formed of the lower rear portion of the wing and were rotated downward about axes at their front edges.
Harris, Thomas E, Weick, Fred E
core   +1 more source

Influence of Non-Uniform Wall Temperature on Local Heat Transfer Coefficient in a Rotating Square Channel

open access: yesInternational Journal of Industrial Engineering and Production Research, 2007
: This paper presents the results of an experimental examination of the effect of non-uniform wall temperature on local heat transfer coefficient in a rotating smooth-walled square channel.
K. Farhadi
doaj  

Post-flight analyses of the crystals from the M0003-14 quartz crystal microbalance experiment [PDF]

open access: yes
Quartz Crystal Microbalances constructed by QCM Research were flown on the leading and trailing edges of LDEF as one of the sub-experiments of M0003.
Radhakrishnan, G.   +2 more
core   +1 more source

Generalization of analytical tools for helicopter-rotor airfoils [PDF]

open access: yes
A state-of-the-art finite difference boundary-layer program incorporated into the NYU Transonic Analysis Program is described. Some possible treatments for the trailing edge region were investigated.
Gibbs, E. H.
core   +1 more source

Vortex-lift roll-control device [PDF]

open access: yes, 1979
A wing is described for aircraft of cropped, arrow-type planform with thin leading and side edges. The wing has a pivotable tip to alter the crop angle of the wing during flight.
Lamar, J. E.
core   +1 more source

TOPOLOGY OPTIMIZATION OF MORPHING WING TRAILING EDGE BASED ON MULTI-POINTS DRIVING COMPLIANT MECHANISM

open access: yesJixie qiangdu, 2018
The wing is designed by specific flight conditions,and its aerodynamic efficiency under various conditions needs to be optimized.This paper studies the trailing edge of the morphing wing to make it meet the aerodynamic optimal deformation range under the
KOU Xin, GE WenJie
doaj  

On the generation of side-edge flap noise [PDF]

open access: yes
A theory is proposed for estimating the noise generated at the side edges of part span trailing edge flaps in terms of pressure fluctuations measured just in-board of the side edge of the upper surface of the flap.
Howe, M. S.
core   +1 more source

Herbivore Fronts Shape Saltmarsh Plant Traits and Performance

open access: yesEcology and Evolution
Herbivore fronts can alter plant traits (chemical and/or morphological features) and performance via grazing. Yet, herbivore‐driven trait alterations are rarely considered when assessing how these fronts shape ecosystems, despite the critical role that ...
Serina S. Wittyngham, David S. Johnson
doaj   +1 more source

Force and moment measurements on a 74 deg delta wing with an apex flap [PDF]

open access: yes
Results are presented of a subsonic experimental investigation of an apex flap concept on a 74 deg swept delta wing with trailing-edge flaps. The apex flap comprised approximately 6 percent of the wing area forward of a transverse hinge, allowing for ...
Buter, T. A., Rao, D. M.
core   +1 more source

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