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Priority to SU2802907/23ApriorityCriticalpatent/SU797336A1/en
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Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks
(AREA)
Abstract
Устройство для определения аэродинамических характеристик модели летательного аппарата, содержащее идентичные измерительные системы для крепления эталонной и испытываемой моделей летательного аппарата, при этом измерительная система с испытываемой моделью размещена в рабочей части аэродинамической трубы, отличающееся тем, что, с целью повышения точности определения аэродинамических характеристик модели с истекающими струями двигательных установок, устройство снабжено соединенной с рабочей частью трубы камеры, в которой размещена измерительная система с эталонной моделью.A device for determining the aerodynamic characteristics of an aircraft model containing identical measuring systems for attaching the reference and tested models of an aircraft, while the measuring system with the model being tested is located in the working part of the wind tunnel, characterized in flowing streams of propulsion systems, the device is equipped with a chamber connected to the working part of the chamber in which and a measuring system with a reference model.
SU2802907/23A1979-07-301979-07-30
DEVICE FOR DETERMINING AERODYNAMIC CHARACTERISTICS OF AIRCRAFT MODEL
SU797336A1
(en)
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Research on noise generated by ducted air-fuel combustion systems(Research facility for studying noise generated by bluff body flow interaction inside ducted fuel combustion system)[Annual Report, 1 Mar. 1971- 29 Feb. 1972]
A wind tunnel flight correlation of Apollo 16 sonic boom(Correlation of sonic boom pressure signatures recorded during reentry of Apollo 16 command module with wind tunnel signatures)
Forward velocity effects on fan noise and the influence of inlet aeroacoustic design as measured in the NASA Ames 40 x 80 foot wind tunnel[Technical Report, 8 Nov. 1979- 31 Jan. 1981]
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