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1
Drag reduction obtained by modifying a standard truck /
Published 1978CONNECT
Government Document Electronic eBook -
2
Mechanism of water droplet breakup near the leading edge of an airfoil /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
3
Optimization of low-thrust spiral trajectories by collocation /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
4
A non-cut cell immersed boundary method for use in icing simulations /
Published 2013CONNECT
Government Document Electronic eBook -
5
Hydrogen-bonding surfaces for ice mitigation /
Published 2014CONNECT
Government Document Electronic eBook -
6
Minimum-cost aircraft descent trajectories with a constrained altitude profile /
Published 2015CONNECT
Government Document Electronic eBook -
7
Guide to AERO2S and WINGDES computer codes for prediction and minimization of drag due to lift /
Published 1997CONNECT
Government Document Electronic eBook -
8
Dynamic ground effect for a cranked arrow wing airplane /
Published 1997CONNECT
Government Document Electronic eBook -
9
Flexible micropost arrays for shear stress measurement /
Published 2015CONNECT
Government Document Electronic eBook -
10
A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program /
Published 1999CONNECT
Government Document Electronic eBook -
11
Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment /
Published 1999CONNECT
Government Document Electronic eBook -
12
Flight test of an adaptive configuration optimization system for transport aircraft /
Published 1999CONNECT
Government Document Electronic eBook -
13
Model engine performance measurement from force balance instrumentation /
Published 1998CONNECT
Government Document Electronic eBook -
14
Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness /
Published 2001CONNECT
Government Document Electronic eBook -
15
Generation of performance model for the Aeolian Wind Tunnel (AWT) rotor at reduced pressure /
Published 2018CONNECT
Government Document Electronic eBook -
16