A Green's function formulation for a nonlinear potential flow solution applicable to transonic flow [PDF]
Routine determination of inviscid subsonic flow fields about wing-body-tail configurations employing a Green's function approach for numerical solution of the perturbation velocity potential equation is successfully extended into the high subsonic ...
Baker, A. J., Fox, C. H., Jr.
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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
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Energy efficient transport technology: Program summary and bibliography [PDF]
The Energy Efficient Transport (EET) Program began in 1976 as an element of the NASA Aircraft Energy Efficiency (ACEE) Program. The EET Program and the results of various applications of advanced aerodynamics and active controls technology (ACT) as ...
Bartlett, D. W. +2 more
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Numerical and experimental study of aerosol dispersion in the Do728 aircraft cabin. [PDF]
CEAS Aeronaut J, 2023 Schmeling D +3 more
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PAN AIR summary document (version 1.0) [PDF]
The capabilities and limitations of the panel aerodynamics (PAN AIR) computer program system are summarized. This program uses a higher order panel method to solve boundary value problems involving the Prandtl-Glauert equation for subsonic and supersonic
Derbyshire, T., Sidwell, K. W.
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Influence of Holes Manufacture Technology on Perforated Plate Aerodynamics. [PDF]
Materials (Basel), 2021 Grzelak J, Szwaba R.
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Unsteady aerodynamic analysis of space shuttle vehicles. Part 1: Summary report [PDF]
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show that slender wing theory can be modified to give the potential flow static and dynamic characteristics over a large Mach number range from M = 0 to M 1. A
Ericsson, L. E., Reding, J. P.
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Wind tunnel wall interference in V/STOL and high lift testing: A selected, annotated bibliography [PDF]
This bibliography, with abstracts, consists of 260 citations of interest to persons involved in correcting aerodynamic data, from high lift or V/STOL type configurations, for the interference arising from the wind tunnel test section walls.
Cole, K. L. +2 more
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A parallel methodology of adaptive Cartesian grid for compressible flow simulations. [PDF]
Adv Aerodyn, 2022 Qi X, Yang Y, Tian L, Wang Z, Zhao N.
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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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