Effect of blockage ratio on drag and pressure distributions for bodies of revolution at transonic speeds [PDF]
Experimental data were obtained in two wind tunnels for 13 models over a Mach number range from 0.70 to 1.02. Effects of increasing test-section blockage ratio in the transonic region near a Mach number of 1.0 included change in the shape of the drag ...
Brooks, C. W., Jr., Couch, L. M.
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Supersonic cruise aircraft research: An annotated bibliography [PDF]
This bibliography, with abstracts, consists of 69 publications arranged in chronological order. The material may be useful to those interested in supersonic cruise fighter/penetrator/interceptor airplanes.
Tuttle, M. H.
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Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology [PDF]
This bibliography, with abstracts, consists of 298 citations arranged in chronological order. The citations were selected to be helpful to persons engaged in the design and development of quiet (low disturbance) nozzles for modern supersonic wind tunnels.
Wolf, Stephen W. D.
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Prediction of forces and moments for flight vehicle control effectors: Workplan [PDF]
Two research activities directed at hypersonic vehicle configurations are currently underway. The first involves the validation of a number of classical local surface inclination methods commonly employed in preliminary design studies of hypersonic ...
Maughmer, Mark D.
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Aeronautical Engineering. A continuing bibliography, supplement 115 [PDF]
This bibliography lists 273 reports, articles, and other documents introduced into the NASA scientific and technical information system in October ...
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Aerodynamic Effects of a Blended Multi-Winglet on an Airliner in Subsonic and Transonic Regimes. [PDF]
Biomimetics (Basel)Kobayashi E +3 more
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Multi-Fidelity Aerodynamic Data Fusion with a Deep Neural Network Modeling Method. [PDF]
Entropy (Basel), 2020 He L, Qian W, Zhao T, Wang Q.
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Advanced aerodynamics and active controls technology [PDF]
The results, status, and plans of NASA sponsored advanced aerodynamics and active controls technology activities are reported.
Alford, W. J., Jr.
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Weak wall boundary conditions for compressible flows. [PDF]
Eng ComputJaiswal M +4 more
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A critical assessment of wind tunnel results for the NACA 0012 airfoil [PDF]
A large body of experimental results, obtained in more than 40 wind tunnels on a single, well-known two-dimensional configuration, has been critically examined and correlated.
Mccroskey, W. J.
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