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1
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2
A Method for calculating laminar viscous, compressible flows with small pressure gradients /
Published 1972CONNECT
Government Document Electronic eBook -
3
The effect of curvature on the transition from laminar to turbulent boundary layer /
Published 1937CONNECT
Government Document Electronic eBook -
4
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5
An analysis of the Bernoulli lift effect as a propulsive component of swimming strokes
Published 1991Thesis Microfilm Book -
6
Energy cost of walking/jogging in a laminar flow resistance pool
Published 1997Thesis Microfilm Book -
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8
Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade /
Published 2012CONNECT
Government Document Electronic eBook -
9
Laminar hydraulic analysis of a commercial pressurized water reactor assembly /
Published 2013CONNECT
Government Document Electronic eBook -
10
Aerodynamic design of a propeller for high-altitude balloon trajectory control /
Published 2012CONNECT
Government Document Electronic eBook -
11
Inverse boundary-layer theory and comparison with experiment /
Published 1978CONNECT
Government Document Electronic eBook -
12
Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove /
Published 2014CONNECT
Government Document Electronic eBook -
13
A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations /
Published 1980CONNECT
Government Document Electronic eBook -
14
Flight tests of a supersonic natural laminar flow airfoil /
Published 2015CONNECT
Government Document Electronic eBook -
15
Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue /
Published 1980CONNECT
Government Document Electronic eBook -
16
Numerical flow visualization in basic- and hyper-cluster spheres /
Published 1997CONNECT
Government Document Electronic eBook -
17
Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /
Published 1990CONNECT
Government Document Electronic eBook -
18
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
Published 1997CONNECT
Government Document Electronic eBook -
19
Visualization of flows in packed beds of twisted tapes /
Published 2002CONNECT
Government Document Electronic eBook -
20
Subsonic ultra green aircraft research phase II-volume I-3 /
Published 2014CONNECT
Government Document Electronic eBook