Results 61 to 70 of about 10,561 (136)

Wind tunnel wall interference in V/STOL and high lift testing: A selected, annotated bibliography [PDF]

open access: yes
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
core   +1 more source

Solution of transonic flows by an integro-differential equation method [PDF]

open access: yes
Solutions of steady transonic flow past a two-dimensional airfoil are obtained from a singular integro-differential equation which involves a tangential derivative of the perturbation velocity potential.
Ogana, W.
core   +1 more source

Raman temperature and density measurements in supersonic jets. [PDF]

open access: yesExp Fluids, 2021
Wernet MP, Georgiadis NJ, Locke RJ.
europepmc   +1 more source

Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing [PDF]

open access: yes
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
core   +1 more source

VUV to IR Emission Spectroscopy and Interferometry Diagnostics for the European Shock Tube for High-Enthalpy Research. [PDF]

open access: yesSensors (Basel), 2023
Grosso Ferreira R   +6 more
europepmc   +1 more source

Aeronautical engineering: A continuing bibliography with indexes, supplement 100 [PDF]

open access: yes
This bibliography lists 295 reports, articles, and other documents introduced into the NASA Scientific and Technical Information System in August ...

core   +1 more source

Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft [PDF]

open access: yes
The aerodynamic performance of V/STOL and STOVL fighter/attack aircraft was assessed. Aerodynamic and propulsion/airframe integration activities are described and small and large scale research programs are considered. Uncertainties affecting aerodynamic
Nelms, W. P.
core   +1 more source

Critical review of the trailing edge condition in steady and unsteady flow. Blade flutter in compressors and fans: Numerical simulation of the aerodynamic loading [PDF]

open access: yes
Existing interpretations of the trailing edge condition, addressing both theoretical and experimental works in steady, as well as unsteady flows are critically reviewed.
Johnson, S. H.   +2 more
core   +1 more source

Reynolds number effects on the transonic aerodynamics of a slender wing-body configuration [PDF]

open access: yes
Aerodynamic forces and moments for a slender wing-body configuration are summarized from an investigation in the Langley National Transonic Facility (NTF).
Cundiff, Jeffrey S.   +2 more
core   +1 more source

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