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1
Mechanism of water droplet breakup near the leading edge of an airfoil /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
2
Droplet deformation prediction with the Droplet Deformation and Breakup Model (DDB) /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
3
Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /
Published 2013CONNECT
Government Document Electronic eBook -
4
Composite Crew Module (CCM) permeability characterization /
Published 2013CONNECT
Government Document Electronic eBook -
5
Delay of transition using forced damping /
Published 2014CONNECT
Government Document Electronic eBook -
6
Computer program to obtain ordinates for NACA airfoils /
Published 1996CONNECT
Government Document Electronic eBook -
7
Ultra high temperature (UHT) SiC fiber (phase II) /
Published 2015CONNECT
Government Document Electronic eBook -
8
Flight demonstration of a shock location sensor using constant voltage hot-film anemometry /
Published 1997CONNECT
Government Document Electronic eBook -
9
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber /
Published 1996CONNECT
Government Document Electronic eBook -
10
Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
Published 1996CONNECT
Government Document Electronic eBook -
11
Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /
Published 1990CONNECT
Government Document Electronic eBook -
12
Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program /
Published 1997CONNECT
Government Document Electronic eBook -
13
A thermostructural analysis of a diboride composite leading edge /
Published 1996CONNECT
Government Document Electronic eBook -
14
Space shuttle pinhole formation mechanism studies /
Published 1998CONNECT
Government Document Electronic eBook -
15
Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /
Published 2017CONNECT
Government Document Electronic eBook -
16
Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters /
Published 1988CONNECT
Government Document Electronic eBook -
17
Jet surface interaction, scrubbing noise /
Published 2013CONNECT
Government Document Electronic eBook