Skin-Friction-Based Identification of the Critical Lines in a Transonic, High Reynolds Number Flow via Temperature-Sensitive Paint. [PDF]
Sensors (Basel), 2021 Costantini M +3 more
europepmc +1 more source
Flutter of a Low-Aspect-Ratio Rectangular Wing [PDF]
A flutter test of a low-aspect-ratio rectangular wing was conducted in the Langley Transonic Dynamics Tunnel (TDT). The model used in this flutter test consisted of a rigid wing mounted to the wind-tunnel wall by a flexible, rectangular beam.
Cole, Stanley R.
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Numerical study on the influence of wall temperature gradient on aerodynamic characteristics of low aspect ratio flying wing configuration. [PDF]
Sci Rep, 2021 Lin P +6 more
europepmc +1 more source
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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External store effects on the stability of fighter and interceptor airplanes [PDF]
Some criteria for external carriage of missiles for fighter aircraft intended for aerial combat missions and for fighter-interceptor missions are considered.
Sawyer, W. C., Spearman, M. L.
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Materials and construction techniques for cryogenic wind tunnel facilities for instruction/research use [PDF]
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are presented to provide a starting point for the design of an instructional/research wind tunnel facility.
Morse, S. F., Roper, A. T.
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Road to Acquisition: Preparing a MEMS Microphone Array for Measurement of Fuselage Surface Pressure Fluctuations. [PDF]
Micromachines (Basel), 2021 Ahlefeldt T +4 more
europepmc +1 more source
Review of aerodynamic design in the Netherlands [PDF]
Aerodynamic design activities in the Netherlands, which take place mainly at Fokker, the National Aerospace Laboratory (NLR), and Delft University of Technology (TUD), are discussed.
Labrujere, Th. E.
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A Review of Riemann Solvers for Hypersonic Flows. [PDF]
Arch Comput Methods Eng, 2022 Qu F, Sun D, Liu Q, Bai J.
europepmc +1 more source
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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