Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing [PDF]
The flow over the B-1 wing is studied computationally, including the aeroelastic response of the wing. Computed results are compared with results from wind tunnel and flight tests for both low-sweep and high-sweep cases, at 25.0 deg.
Goorjian, P. M. +3 more
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Aeronautical Engineering: A special bibliography with indexes, supplement 67, February 1976 [PDF]
This bibliography lists 341 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...
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Wall interference assessment and corrections [PDF]
Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical results are discussed in terms of several nonlinear transonic codes and one panel method code developed for and being implemented at NASA-Langley ...
Garriz, J. A. +2 more
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Energy Stability Property of the CPR Method Based on Subcell Second-Order CNNW Limiting in Solving Conservation Laws. [PDF]
Entropy (Basel), 2023 Liu R, Yan ZG, Zhu H, Jia F, Feng X.
europepmc +1 more source
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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An Ultra-Fast TSP on a CNT Heating Layer for Unsteady Temperature and Heat Flux Measurements in Subsonic Flows. [PDF]
Sensors (Basel), 2022 Bitter M +4 more
europepmc +1 more source
Adaptive wall wind tunnels: A selected, annotated bibliography [PDF]
This bibliography, with abstracts, consists of 257 citations arranged in chronological order. Selection of the citations was made for their value to researchers working to solve problems associated with reducing wall interference by the design ...
Mineck, R. E., Tuttle, M. H.
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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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Characterization of Supersonic Compressible Fluid Flow Using High-Speed Interferometry. [PDF]
Sensors (Basel), 2021 Psota P +10 more
europepmc +1 more source
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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