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3 edition of Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment found in the catalog.

Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment

Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment

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  • 35 Currently reading

Published by Princeton University, National Aeronautics and Space Administration, Langley Research Center in Princeton, N.J, Hampton, Va .
Written in English

    Subjects:
  • Space vehicles -- Atmospheric entry.,
  • Flow distribution.,
  • Mass spectroscopy.,
  • Raman spectra.,
  • Space Shuttle orbiters.

  • Edition Notes

    StatementR. B. Miles, D. A. Santavicca, and M. Zimmermann.
    SeriesNASA contractor report -- 172142., NASA contractor report -- NASA CR-172142.
    ContributionsSantavicca, D. A., Zimmermann, Mosche., Princeton University., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18295897M

    2 - Report the difference between what you've experimentally measured and what the simulation predicted. Are they within the expected sensitivity of the instrument? The difference between what we experimentally measured and what the simulation predicted was gram. Many industrial processes are plagued by particulate materials traveling through enclosures such as pipes and machines. Solutions to Erosion-based sand management have historically employed an intrusive inserted sensor into the pipe’s flow-stream. However, more recent solutions have employed acoustic-based techniques to measure sand production by monitoring the sand’s . Measurement of the spectral absorption coefficient in the ocean with an isotropic source Robert A. Maffione, Kenneth J. Voss, and Richard C. Honey Closed-form equations that describe the vector irradiance from an isotropic source embedded in the ocean are rigorously derived from the steady-state radiative transfer equation. Aircraft icing is widely recognized as a significant hazard to aircraft operations in cold weather. When an aircraft or rotorcraft fly in a cold climate, some of the super-cooled water droplets would impact and freeze on the exposed aircraft surfaces to form ice shapes, which can degrade the aerodynamic performance of an airplane significantly by decreasing lift while increasing drag, Author: Haixing Li.

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Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment Download PDF EPUB FB2

Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment Article (PDF Available) October with 19 Reads How we measure 'reads'. Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment Author: Richard B Miles ; D A Santavicca ; M Zimmermann ; Princeton University.

EVALUATION OF NON-I NTRUSIVE FLOW MEASUREMENT TECHNIQUES FOR A RE-ENTRY FLIGHT EXPERIMENT R. Miles, D. Santavicca, and M. Zimmermann Abstract This study evaluates various non-intrusive techniques for the measure- ment of the flow field on the windward side of the Space Shuttle orbiter or a similar re-entry vehicle.

Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment. By D. Santavicca, R. Miles and M. Zimmermann. Abstract. This study evaluates various non-intrusive techniques for the measurement of the flow field on the windward side of the Space Shuttle orbiter or a similar reentry vehicle.

Included are linear. EVALUATION OF NON-INTRUSIVE FLOW MEASUREMENT TECHNIQUES FOR A RE-ENTRY FLIGHT EXPERIMENT I?. MILES, D. SANTAVICCA, AND M. ZIMMERMANN Princeton University Princeton, New Jersey Cooperative Agreement NCCI NOVEMBER File Size: 7MB. requires reliable flow measurement of the oil.

Before non-intrusive ultrasonic flow measurement technology was introduced, the flow was determined by means of differential pressure measurement. Operations had to be stopped once a year in order to carry out the inspection and maintenance of the system. The medium is a car-cinogenic substance.

Gas holdup and solids concentration measurement methods can be classified into two categories: those providing an overall or global measurement and those that provide a local or point measurement. The global measuring techniques yield information on the line, area or volume averaged gas or solids holdup.

Boden, Fritz und Kirmse, Tania und Weikert, Thorsten und Wolf, Thomas und Petit, C. und Jentink, H.W. () Application of a new optical Measurement Technique for Non-Intrusive Wing Deformation Measurement on a Large Transport Aircraft.

21th SFTE (EC) Symposium, 3. - 6. OctoberVergiate (VA) Italy. Dieses Archiv kann nicht den gesamten Text zur Verfügung Cited by: 4.

Abstract. The transport of payload into space, either suborbital, orbital or superorbital and its return to the Earth’s surface, is known to require the development and construction of suitable vehicles which are able to withstand the very severe thermal and mechanical (pressure and shear stress) loads encountered Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment book such a by: 1.

for mining applications: Understanding and selecting the right technology for the application. This paper will only review non-invasive flow meter technologies (time of flight ultrasonic, Doppler ultrasonic, and array-based sonar), their maintenance requirements, and their pros and cons when flow measurement elements.

Noeding, P. und Bregman, E. und Longo, J.M.A. () Assessment of Aerothermodynamic Analysis Methods with Regard to the Planned SHEFEX Flight Experiment.

In: 4th International Symposium Atmospheric Reentry Vehicles & Systems Proceedings. 4th International Symposium Atmospheric Reentry Vehicles & Systems, [ - ], Arcachon, : P.

Noeding, E. Bregman, J.M.A. Longo. This study evaluates various non-intrusive techniques for the measurement of the flow field on the windward side of the Space Shuttle orbiter or a similar reentry vehicle.

American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Flush Airdata Sensing systems use non-intrusive surface pressure measurements to infer vehicle position, speed, and orientation.

This paper presents the design procedure and preliminary test results for a simplified flush airdata sensing system for the uncontrolled hypersonic flight experiment HIFiRE by: 2.

These optical methods, besides being non-intrusive and giving a global view of the flow field, as do all methods of visualization, have peculiar advantages and disadvantages: The inertia of the system is practically zero, the study of unsteady motions is possible with the temporal discrimination allowed by the speed of the shut-off system.

It is primarily intended for engineers, scientists and students, who already have some basic knowledge of fluid mechanics and non-intrusive optical measurement techniques. It shall guide researchers and engineers to design and perform their experiment successfully without requiring them to first become specialists in the : Springer International Publishing.

RS Hydro launch a new steam flow measurement and survey service. Equipment Used. The Panametrics PTGC Portable Flow Meter. Background. Manufacturers the world over have been asked repeatedly whether there is a non-invasive steam flow meter system for measuring steam flow rates.

AIAA Atmospheric Flight Mechanics Conference and Exhibit. 16 August - 19 August Providence, Rhode Island Evaluation of Wavelet-Based Techniques for Detecting Loss of Control.

David Klyde, Peter Thompson, Deflection Measurement Accuracy in a Course-Corrected mm Mortar Spark Range Flight Experiment. Bernard Guidos. Craig T. Johansen's Google Scholar Profile Craig T. Johansen's Research Gate Profile Journal Publications (Peer J., and Cruden, B.A., () “Non-intrusive measurement techniques for flow characterization of hypersonic wind tunnels,” manuscript and presentation in Lecture Series: “Flow Characterization and Modeling of Hypersonic Wind.

3 Why Discuss This Are Here Typical test engineers—talented “ those smart guys ” Within discipline (AE, EE, ME, CE) and generally in flight testing Technical experts However—limited knowledge in test design alpha, beta, sigma, delta, p, & n or N Test design is not an art it is a science Make decisions too important to be left to professional.

Non‐Intrusive Techniques Emission Spectroscopy. RESPECT, PHLUX, COMPARE) Description of PYREX‐KAT38 (Pyrometric Entry Experiment) RESPECT (Re‐Entry SPECTrometer) COMPARE.

Numerical Simulation of Flow Fields Past Space Transportation Systems Temperature and Heatflux Measurement. Force and Moment Measurement. Flow Cited by: 1. methods for actual hypersonic flight conditions because wind-tunnel testing has not been historically feasible, e.g.

Bertilrud, et al. 1 Crucial to the success of the experiment is the ability to design, analyze, and fabricate a fully-instrumented flight-test fixture that can provide a smooth, three-dimensional, structurally stable aerodynamicCited by: 3.

When exposed to a plasma flow, the material undergoes pyrolysis and ablation, and various chemical species enter the gas phase where they may combine with the species present in the plasma.

The products in the gas phase can be detected by non-intrusive optical diagnostic techniques, as described in this section.

Basic Principles of Flight Test Instrumentation Engineering (AGARDographVolume 1, Issue 2) [Borek, R.W.; Pool, A. (eds.)] on *FREE* shipping on qualifying offers. Basic Principles of Flight Test Instrumentation Engineering (AGARDographPrice: $ The temperature dependence of the recombination coefficient is explained by elementary reaction steps.

Furthermore, the reaction scheme established is implemented in a two-dimensional Navier–Stokes code computing the re-entry flow around a simple geometry to show the importance of a detailed modeling of surface by: IEEE offers subscription options to suit any size organization; ranging from large universities to small companies.

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Whether you are an academic institution that. T1 - Detached eddy simulation of the Reentry-F flight experiment. AU - Barnhardt, Michael. AU - Candler, Graham V. PY - /12/1. Y1 - /12/1.

N2 - Results of detached eddy simulations of the Reentry-F vehicle are presented and compared to the experimental by: 4. -- A new electronic type of flapping-wing aircraft -- Restoring a complex heritage aircraft to flight: some observations from the re-introduction of innovative but obsolete 20th century technologies into a risk-averse 21st century regulatory environment -- Flying car design and testing -- Temperature measurement of rotating turbo-machinery.

Title: Techniques Used in the F Variable-Sweep Transition Flight Experiment Author: Bianca Trujillo Anderson, Robert R. Meyer, Jr., and Harry R. Chiles. PNA equipment can be easily installed at different loops, and PNA techniques are non-intrusive and independent of flow regimes.

These features of the PNA technique make it suitable for in-situ measurement of two-phase flows, and for calibration of more conventional two-phase flow measurement devices. The test objects and methods used to measure leeway in these studies are reviewed.

The leeway guidance of the present U.S. Coast Guard search planning tools is also reviewed. A comparison between an older leeway data set and a recent leeway data set is used to illustrate recent gains in our understanding of leeway behavior. The Importance of Respiratory Rate Monitoring.

Before dealing with the f R methods, we briefly describe the major applications where the monitoring of f R is invaluable. A further aim is to increase awareness of the importance of measuring fdespite a large body of evidence indicating that f R is a very relevant vital sign that responds to a variety of Cited by: @article{osti_, title = {Mass flow measurement of solids/gas stream using radiometric techniques}, author = {Linn, J.

and Sample, D. G.}, abstractNote = {A mass flowmeter utilizing radiometric techniques has been designed and built for measuring flows in two phase gas/solids feed streams in coal gasification processes.

The instrument combines a radiometric density measurement. Control Engineering and Information Systems contains the papers presented at the International Conference on Control Engineering and Information Systems. Control Engineering and Information Systems book. On counter-measure to flight colleges modern long-distance education existing state and : Zhijing Liu.

Application of Design of Experiments to Flight Test: A Case Study. Major Aaron A. Tucker. United States Air Force, Edwards Air Force Base CA Gregory T. Hutto. Un ited States Air Force, Eglin Air Force Base FL and Cihan H. Dagli. University of M issouri -Rolla, Rolla MO Cited by: Refraction of sound by jet flow and jet temperature: Extension of temperature range parameters and development of theory (NASA contractor report) [Grande, E] on *FREE* shipping on qualifying offers.

Refraction of sound by jet flow and jet temperature: Extension of temperature range parameters and development of theory (NASA contractor report)Author: E Grande. Biology, Earth science, Physics, Chemistry, Social science. The group that does not receive the experimental treatment in an experiment is the.

Control group. Which step in the experimental method are scientists conducting when they photograph birds in flight. observing. The International Space Station (ISS) is a modular space station (habitable artificial satellite) in low Earth ISS programme is a multi-national collaborative project between five participating space agencies: NASA (United States), Roscosmos (Russia), JAXA (Japan), ESA (Europe), and CSA (Canada).

The ownership and use of the space station is established by Crew: Fully crewed: 6, Currently aboard:. This proceedings book presents the results of the 31st International Symposium on Shock Waves (ISSW31), held in Nagoya, Japan in It covers among others blast waves, chemical reacting flows, chemical kinetics, detonation and combustion, flow.

To study the wall jet in counter-flow, it is important to understand the behavior of a free jet in counter-flow. It is the flow of a jet in an opposing stream when the jet exit velocity (U. j) is greater than the velocity of the opposed current (U. Figure 2 shows a schematic of a free round jet with diameter.

in a uniform counter-flow. Purchase Automatic Control in Aerospace - 1st Edition. Print Book & E-Book. ISBNBook Edition: 1.NASA planned to have a Space Shuttle dock with it, and elevate Skylab to a higher safe altitude, but the Shuttle was not ready for flight before Skylab's re-entry on J [58] To save cost, NASA used one of the Saturn V rockets originally earmarked for a canceled Apollo mission to launch the iction: US Federal Government.That is, a measure in which any two adjoining values are the same distance apart and there is a true zero point.

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