2 edition of Heat-transfer measurements in short-duration hypersonic facilities found in the catalog.
Heat-transfer measurements in short-duration hypersonic facilities
Donald Lorimer Schultz
|Statement||by D.L. Schultz and T.V. Jones.|
|Series||AGARDograph -- no.165|
|Contributions||Jones, T V., Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel.|
|The Physical Object|
|Number of Pages||149|
Principles of Hypersonic Test Facility Development Control of the System and Measurement Equipment of AT driven section driver gas dynamic energy addition engine enthalpy flight conditions flowfield ground test guideway heat flux heat transfer helium high-enthalpy high-pressure hypersonic test Hypersonic Wind Tunnel. Books. An illustration of two cells of a film strip. Video An illustration of an audio speaker. DTIC ADA Force Measurements in Short-Duration Hypersonic Facilities Item Preview remove-circle Force Measurements in Short-Duration Hypersonic Facilities by Defense Technical Information Center.
A method has been developed which applies liquid-crystal thermography to the measurement of surface heat flux in short-duration hypersonic facilities. Flat-plate thermographs are compared with Eckert's prediction of surface heat flux to provide a calibration which replaces the liquid-crystal static color calibration. Book Search tips Selecting this option will search all publications across the Scitation platform Selecting this option will search all publications for the Publisher/Society in context. “ Heat–transfer measurements in short–duration hypersonic facilities,” AGARDograph
COVID Resources. Reliable information about the coronavirus (COVID) is available from the World Health Organization (current situation, international travel).Numerous and frequently-updated resource results are available from this ’s WebJunction has pulled together information and resources to assist library staff as they consider how to handle . heat transfer measurements in hypersonic ﬂow experiments. This approach has been used with reasonable success in long duration test facilities like hypersonic wind tunnels where the reservoir conditions can be easily controlled during experiments. On the other hand, in short.
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Camci, C. and Arts, T. () Short duration heat transfer measure- ments, in von Karman Institute Lecture Series on Measurement T echniques in Turbomachines, Author: Cengiz Camci.
Buy Heat-transfer measurements in short-duration hypersonic facilities, (AGARDograph) by Schultz, Donald Lorimer (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Donald Lorimer Schultz.
Heat-transfer measurements in short-duration hypersonic facilities. [Neuilly sur Seine] North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Heat-transfer measurements in short-duration hypersonic facilities book  (OCoLC) Accession Number: AD Title: Heat-Transfer Measurements in Short-Duration Hypersonic Facilities.
Descriptive Note: AGARDograph rept., Corporate Author: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE) Personal Author(s): Schultz,D. ; Jones,T. Report Date: FEB Pagination or Media Count: Cited by: Heat-transfer measurements were made in both test gases on 70 deg sphere-cone models and on hemisphere models of various radii.
HYPULSE freestream flow conditions in these test gases were found to be repeatable to within ±%, and aerothermodynamic test times of µsec in CO 2 and µsec in air were identified. Abstract: This is the first of several AGARDographs commissioned by the Fluid Dynamics Panel to deal with instrumentation techniques used in hypersonic short-duration facilities and with related topics.
Since one of the reasons for the development of such facilities was the need for experimental data on the extremely high heat-transfer rates that a body experiences in re. Measurement Techniques in Hypersonic Facilities Conventional Techniques Bernstein  produced a comprehensive review of the force measurement techniques and force balances used in short-duration facilities during the period Schultz D L and Jones T V Heat-transfer measurements in short-duration hypersonic facilities AGARDograph no North Atlantic Treaty Organisation Thorpe S J, Yoshino S and Ainsworth R W Fabrication and calibration techniques for turbine rotor tip heat transfer gauges 15th Symposium on Measuring Techniques in Transonic and.
A technique for fast-response surface temperature measurement of an electrically preheated carbon-phenolic model using an indium gallium arsenide detector with in situ calibration via a visible/near-infrared spectrometer is assessed through application in a short-duration cold-flow hypersonic wind tunnel.
Magnetohydrodynamic (MHD) aerobraking has the potential to significantly reduce peak heat loads for high-speed planetary entry, due to increases in total drag force in the early phase of the trajectory.
Establishing accurate techniques for measuring MHD drag force in ground testing facilities is a necessary first step for investigating this phenomenon. Introduction. Stagnation temperature, and the fluctuation thereof, can have a significant impact in many hypersonic flow experiments, but due to the impulsive loading and short test times in many facilities, these parameters can be difficult to such facility with short duration flows which commence and terminate rapidly is TUSQ, a hypersonic Ludwieg tube facility.
The development and application of high-speed imaging and luminescent coating techniques to measure full-field surface heat-transfer rates in short-duration hypersonic flow is presented. Abstract. Measurement techniques routinely used at the NASA Langley Research Center to obtain qualitative and quantitative global and discrete values of heat transfer rate to the surface of models tested in conventional-type hypersonic wind tunnels and an impulse facility (NASA Hypulse at the General Applied Science Laboratory) are presented.
Heat transfer rates measured in front and to the side of a protrusion on an aluminum flat plate subjected to hypersonic flow at zero angle of attack are presented for two flow enthalpies of approximately 2 MJ/kg and MJ/kg.
Giles, H.L. and Thomas, J.W. Analysis of hypersonic pressure and heat transfer tests on a flat plate with a flap and a delta wing with body, elevons, fins, and rudders,NASA CR Stainback, P.C. and Weinstein, L.M. Aerodynamic heating in the vicinity of corners at hypersonic speeds,NASA TN D Laser Based Calibration Technique of Thin Film Gauges for Short Duration Transient Measurements J.
Thermal Sci. Eng. Appl (December, ) Heat Transfer From a Small Heated Region to R and FC Schultz, D. & Jones, T. Heat-transfer measurements in short-duration hypersonic facilities.
AGARD Technical Report Advisory Group for Aerospace Research and Development. Simmons, J. Measurement techniques in high-enthalpy hypersonic facilities. Exp. Therm. Ireland P T and Jones T V Detailed measurements of heat transfer on and around a pedestal in fully developed passage flow Proc.
Int. Heat Transfer Conf. vol 3, pp Jones T V The thin film heat transfer gauges-a history and new developments 4th National UK Heat Transfer Conf., Manchester (London: ImechE) pp Schultz and T.
Jones, “ Heat-transfer measurements in short-duration hypersonic facilities,” in AGARDograph No.AGARD. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA.
A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer.
Ten chapters address: general characterization of hypersonic flows; basic 3/5(1).Audio Books & Poetry Community Audio Computers, Technology and Science Music, Arts & Culture News & Public Affairs Non-English Audio Spirituality & Religion Librivox Free Audiobook YouTube Power Hour Podcast: YouTube, YouTube Channel, Video Marketing, YouTuber, IGTV, Erika Vieira, Video, Instagram KELLY-kun ElectraTone Guitar Effects.A Six Component Balance for Short Duration Hypersonic Facilities.
Heat Transfer Measurement Techniques Used or in Development at ONERA/Chalais-Meudon. Pages Consigny, H. (et al.) Preview Buy Chap95 € Aerothermodynamic Measurement Techniques Employed in NASA Langley Hypersonic Facilities.