Relevant bibliographies by topics / Compressible flow

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Compressible flow'

Author: Grafiati
Published: 4 June 2021
Last updated: 26 April 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Compressible flow.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Compressible flow"

1

Anwar-ul-Haque, Ning Qin, and Farooq Umar. "ASYMMETRY OF FLOW AT HIGH ANGLE OF ATTACK(Compressible Flow)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 661–66. http://dx.doi.org/10.1299/jsmeicjwsf.2005.661.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

M, Uma. "Flow Pattern of Compressible Fluids in Steady State." International Journal of Science and Research (IJSR) 12, no. 1 (January 5, 2023): 1233–37. http://dx.doi.org/10.21275/sr231010132523.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Veress, Árpád, János Molnár, and József Rohács. "Compressible viscous flow solver." Periodica Polytechnica Transportation Engineering 37, no. 1-2 (2009): 77. http://dx.doi.org/10.3311/pp.tr.2009-1-2.13.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Ockendon, Hilary, and John R. Ockendon. "Waves and Compressible Flow." Applied Mechanics Reviews 57, no. 6 (2004): B33. http://dx.doi.org/10.1115/1.1849177.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Grotberg, J. B., and T. R. Shee. "Compressible-flow channel flutter." Journal of Fluid Mechanics 159, no. -1 (October 1985): 175. http://dx.doi.org/10.1017/s0022112085003160.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Liu, Tai-Ping, Zhouping Xin, and Tong Yang. "Vacuum states for compressible flow." Discrete & Continuous Dynamical Systems - A 4, no. 1 (1998): 1–32. http://dx.doi.org/10.3934/dcds.1998.4.1.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Golubkin, Valerii Nikolaevich, and Grigorii Borisovich Sizykh. "ON THE COMPRESSIBLE COUETTE FLOW." TsAGI Science Journal 49, no. 1 (2018): 29–41. http://dx.doi.org/10.1615/tsagiscij.2018026781.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Molki, Majid. "Introduction to Compressible Fluid Flow." Heat Transfer Engineering 36, no. 5 (October 24, 2014): 521–22. http://dx.doi.org/10.1080/01457632.2014.935227.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Vergassola, M., and M. Avellaneda. "Scalar transport in compressible flow." Physica D: Nonlinear Phenomena 106, no. 1-2 (July 1997): 148–66. http://dx.doi.org/10.1016/s0167-2789(97)00022-5.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

CROWDY, DARREN G. "Compressible bubbles in Stokes flow." Journal of Fluid Mechanics 476 (February 10, 2003): 345–56. http://dx.doi.org/10.1017/s0022112002002975.

Full text
Abstract:
The problem of a two-dimensional inviscid compressible bubble evolving in Stokes flow is considered. By generalizing the work of Tanveer & Vasconcelos (1995) it is shown that for certain classes of initial condition the quasi-steady free boundary problem for the bubble shape evolution is reducible to a finite set of coupled nonlinear ordinary differential equations, the form of which depends on the equation of state governing the relationship between the bubble pressure and its area. Recent numerical calculations by Pozrikidis (2001) using boundary integral methods are retrieved and extended. If the ambient pressures are small enough, it is shown that bubbles can expand significantly. It is also shown that a bubble evolving adiabatically is less likely to expand than an isothermal bubble.
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Compressible flow"

1

Welsh, Stephanie. "Compressible Taylor-Couette flow." Thesis, University of Leeds, 2013. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.616475.

Full text
Abstract:
Incompressible Taylor-Couette flow has been studied extensively over the years. However, the compressible system has been largely ignored with only a few notable studies. The present thesis aims to explore the compressible Taylor-Couette system for a large range of parameters. The compressible equations have been linearised and a spectral method was applied to solve the system using a MATLAB-routine. In Chapter 2, we discuss the analysis performed to solve the system and explain the basic concepts and phenomena we expect to find. We also explain the numerical methods used. Chapter 3 discusses the case in which the outer cylinder remains motionless. The most important parameters, the Mach and Prandtl number and the radius ratio, are varied. In Chapters 4 and 5, the same procedure is applied to the cases of the co- and counter-rotating cylinders, respectively.
APA, Harvard, Vancouver, ISO, and other styles
2

Zwart, Philip J. "Grid turbulence in compressible flow." Thesis, University of Ottawa (Canada), 1996. http://hdl.handle.net/10393/10207.

Full text
Abstract:
The flow downstream of a grid in a wind tunnel is of considerable interest for two reasons. Theoretically, it represents a good approximation to the idealized concept of homogeneous and isotropic turbulence, and therefore provides a benchmark to evaluate various analytical theories of turbulence. On the practical side, grids and screens are used extensively in the management of turbulence in a variety of applications. Experimental studies of grid turbulence are numerous in incompressible flow but far scarcer in compressible flow. The present study considers the characteristics of grid turbulence over a range of Mach numbers, M, ranging from the essentially incompressible (M = 0.16), through the moderate subsonic ($0.16 M 0.7)$ and high subsonic $(0.7 M 1.0),$ to the supersonic (M = 1.55). The experiments comprise flow visualization, performed with the shadowgraph method, and mean and fluctuating velocity measurements, made with a laser-Doppler velocimeter. Characteristics of the flow near the grid were visualized in a demonstration nozzle using the schlieren technique. In the moderate subsonic regime, flow visualization indicated that the flow near the grid underwent major changes as M increased. The turbulence intensity and decay characteristics were also found to be influenced, which was attributed to the changes in the flow near the grid. In the high subsonic regime, an unsteady quasi-normal shock was present in the test section. This induced relatively large velocity fluctuations and anisotropic turbulence. In the supersonic regime, stationary oblique shocks generated by the grid were present throughout the test section, which interfered with the turbulence and introduced errors in the measurement technique.
APA, Harvard, Vancouver, ISO, and other styles
3

Laurantzon, Fredrik. "Flow Measuring Techniques in Steady and Pulsating Compressible Flows." Licentiate thesis, KTH, Mekanik, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-26344.

Full text
Abstract:
This thesis deals with flow measuring techniques applied on steady and pulsatingflows. Specifically, it is focused on gas flows where density changes canbe significant, i.e. compressible flows. In such flows only the mass flow ratehas a significance and not the volume flow rate since the latter depends onthe pressure. The motivation for the present study is found in the use of flowmeters for various purposes in the gas exchange system for internal combustionengines. Applications can be found for instance regarding measurements of airflow to the engine, or measurements of the amount of exhaust gas recirculation.However the scope of thesis is wider than this, since the thesis aims toinvestigate the response of flow meters to pulsating flows. The study is mainlyexperimental, but it also includes an introduction and discussion of several inindustry, common flow measuring techniques.The flow meters were studied using a newly developed flow rig, designedfor measurement of steady and pulsating air flow of mass flow rates and pulsefrequencies typically found in the gas exchange system of cars and smallertrucks. Flow rates are up to about 200 g/s and pulsation frequencies from 0 Hz(i.e. steady flow) up to 80 Hz. The study included the following flow meters:hot-film mass flow meter, venturi flowmeter, Pitot tube, vortex flowmeter andturbine flowmeter. The performance of these meters were evaluated at bothsteady and pulsating conditions. Furthermore, the flow under both steady andpulsating conditions were characterized by means of a resistance-wire basedmass flow meter, with the ability to perform time resolved measurements ofboth the mass flux ρu, and the stagnation temperature T0.Experiments shows that, for certain flow meters, a quasi-steady assumptionis fairly well justified at pulsating flow conditions. This means that thefundamental equations describing the steady flow, for each instant of time,is applicable also in the pulsating flow. In the set-up, back-flow occurred atcertain pulse frequencies, which can result in highly inaccurate output fromcertain flow meters, depending on the measurement principle. For the purposeof finding means to determine when back flow prevails, LDV measurementswere also carried out. These measurements were compared with measurementsusing a vortex flow meter together with a new signal processing technique basedon wavelet analysis. The comparison showed that this technique may have apotential to measure pulsating flow rates accurately.Descriptors: Flow measuring, compressible flow, steady flow, pulsating flow,hot-wire anemometry, cold-wire anemometry.
QC 20101208
APA, Harvard, Vancouver, ISO, and other styles
4

Lanerolle, Lyon Werner John. "Numerical modelling of turbulent compressible flow." Thesis, University of Oxford, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.362004.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Oo, Htet Htet Nwe. "Actuator Disk Theory for Compressible Flow." DigitalCommons@CalPoly, 2017. https://digitalcommons.calpoly.edu/theses/1727.

Full text
Abstract:
Because compressibility effects arise in real applications of propellers and turbines, the Actuator Disk Theory or Froude’s Momentum Theory was established for compressible, subsonic flow using the three laws of conservation and isentropic thermodynamics. The compressible Actuator Disk Theory was established for the unducted (bare) and ducted cases in which the disk was treated as the only assembly within the flow stream in the bare case and enclosed by a duct having a constant cross-sectional area equal to the disk area in the ducted case. The primary motivation of the current thesis was to predict the ideal performance of a small ram-air turbine (microRAT), operating at high subsonic Mach numbers, that would power an autonomous Boundary Layer Data System during test flights. The compressible-flow governing equations were applied to a propeller and a turbine for both the bare and ducted cases. The solutions to the resulting system of coupled, non-linear, algebraic equations were obtained using an iterative approach. The results showed that the power extraction efficiency and the total drag coefficient of the bare turbine are slightly higher for compressible flow than for incompressible flow. As the free-stream Mach increases, the Betz limit of the compressible bare turbine slightly increases from the incompressible value of 0.593 and occurs at a velocity ratio between the far downstream and the free-stream that is lower than the incompressible value of 0.333. From incompressible to a free-stream Mach number of 0.8, the Betz limit increases by 0.021 while its corresponding velocity ratio decreases by 0.036. The Betz limit and its corresponding velocity ratio for the ducted turbine are not affected by the free-stream Mach and are the same for both incompressible and compressible flow. The total drag coefficient of the ducted turbine is also the same regardless of the free-stream Mach number and the compressibility of the flow; but, the individual contributions of the turbine drag and the lip thrust to the total drag differs between compressible and incompressible flow and between varying free-stream Mach numbers. It was concluded that overall compressibility has little influence on the ideal performance of an actuator disk.
APA, Harvard, Vancouver, ISO, and other styles
6

Bonner, Michael Patrick. "Compressible subsonic flow on a staggered grid." Thesis, University of British Columbia, 2007. http://hdl.handle.net/2429/32290.

Full text
Abstract:
This work focuses on numerically modelling the dynamics of a single phase fluid at varying densities and pressures. We explore the potential of incompressible flow simulation methods in modelling compressible flow, with an eye towards computer animation applications. The methods developed capture the interesting thermodynamic effects of compressible flow, and reduce to the standard Marker and Cell incompressible flow Poisson matrix in the incompressible limit. The method works well in modelling flows in the subsonic range that normal incompressible techniques do not capture and where compressible methods are inefficient. We have also investigated adapting these techniques to granular elastic-plastic flow.
Science, Faculty of
Computer Science, Department of
Graduate
APA, Harvard, Vancouver, ISO, and other styles
7

Farooq, Muhammad Asif. "Cartesian Grid Method for Compressible Flow Simulation." Doctoral thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for energi- og prosessteknikk, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-16538.

Full text
Abstract:
The Cartesian grid method is an alternative to the existing methods to solve a physical problem governed by partial differential equations (PDEs) computationally. Researchers are interested in this method due to its simplicity of grid generation,  less computational effort and ease of implementation into a computer code. One of the other options to solve a physical PDE problem is by the body-fitted grid method. In the body-fitted grid method, the boundary points are grid points. This is not the case with the Cartesian grid method where the body wall is embedded as a boundary into a Cartesian grid resultingin irregular cells near the embedded boundary. These irregular cells near the embedded boundary are known as cut-cells. Instead of using special treatmentsof the cut-cells or enforcing the presence of the embedded boundary by adding source terms at the Cartesian grid points near the boundary, the kinematic and other boundary conditions can be introduced in the Cartesian grid method via ghost points. Those grid points which lie inside the embedded boundary and are also a part of computation are called ghost points. Inactive grid points inside the embedded boundary are referred to as solid points. In the present Cartesian grid method, based on a ghost point treatment, local symmetry conditions are imposed at the embedded wall boundary. The ghost point treatments available in the literature are difficult to implement due to complex procedures. We are introducing a new approach to approximate the kinematics of the embedded boundary by a very simple ghost point treatment called the simplified ghost point treatment. In this approach, we consider the grid lines in the x- and y- directions as approximations of the lines normal to the embedded boundary depending on whether the angle between the normal and the x- or y-directions is closer. For 1D hyperbolic nonlinear systems of conservation laws, we use the moving normal shock wave as a test case for the 1D compressible Euler equations.For the 2D compressible Euler equations, we test the simplified ghost point treatment for an oblique shock wave generated by a wedge. Then, we verified our approach for slender bodies, namely for supersonic flow over a circular arc airfoil and for transonic flow over a circular arc bump in a channel. In a final problem, we applied the simplified ghost point treatment to blunt body flow and considered supersonic flows over a cylinder using the 2D compressible Euler and Navier-Stokes equations. The results are good or comparable to those found in the existing literature.
APA, Harvard, Vancouver, ISO, and other styles
8

Lin, Hong-Chia. "Topics in Numerical Computation of Compressible Flow." Thesis, Cranfield University, 1990. http://dspace.lib.cranfield.ac.uk/handle/1826/4555.

Full text
Abstract:
This thesis aims to assist the development of a multiblock implicit Navier-Stokes code for hypersonic flow applications. There are mainly three topics, which concern the understanding of basic Riemann solvers, the implementing of implicit zonal method, and grid adaption for viscous flow. Three problems of Riemann solvers are investigated. The post-shock oscillation problem of slowly moving shocks is examined, especially for Roe's Riemann solver, and possible cures are suggested for both first and second order schemes. The carbuncle phenomenon associated with blunt body calculation is cured by a formula based on pressure gradient, which will not degrade the solutions for viscous calculations too much. The grid-dependent characteristic of current upwind schemes is also demonstrated. Several issues associated with implicit zonal methods are discussed. The effects of having different mesh sizes in different zones when shock present are examined with first order explicit scheme and such effects are shown to be unwanted therefore big mesh size change should be avoided. Several implicit schemes are tested for hypersonic flow. The conservative DDADI scheme is found to be the most robust one. A simple and robust implicit zonal method is demonstrated. A proper treatment of the diagonal Jacobian and choosing the updating method are found to be crucial. The final topic concerns the calculation and grid adaption of viscous flow. We study the linear advection-diffusion equation thoroughly. The results are unfortunately not applicable to Navier-Stokes equations directly. Nevertheless a suggestion on the mesh size control for viscous flow is made and demonstrated. An attempt to construct a cell-vertex TVD scheme is described in the appendix.
APA, Harvard, Vancouver, ISO, and other styles
9

Blank, Henrik. "Numerical methods for compressible and incompressible flow." Thesis, University of Oxford, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.300125.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Wash, Nicholas D. "Upwind iteration techniques for compressible flow computations." Thesis, University of Oxford, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308589.

Full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Books on the topic "Compressible flow"

1

Saad, Michel A. Compressible fluid flow. 2nd ed. Englewood Cliffs, N.J: Prentice Hall, 1993.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
2

Oosthuizen, P. H. Compressible fluid flow. New York: McGraw-Hill, 1997.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
3

Ockendon, Hilary, and John R. Ockendon. Waves and Compressible Flow. New York, NY: Springer New York, 2016. http://dx.doi.org/10.1007/978-1-4939-3381-5.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Palmer, James, Kenneth Ramsden, and Eric Goodger. Compressible Flow Tables for Engineers. London: Macmillan Education UK, 1987. http://dx.doi.org/10.1007/978-1-349-09724-1.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Talwar, Mahesh. Multiphase, compressible, and incompressible flow. Houston: Gulf Pub. Co., Book Division, 1985.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
6

Sayers, A. T. Hydraulic and compressible flow turbomachines. London: McGraw-Hill, 1990.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
7

Hugh L. Dryden Flight Research Center., ed. Unsteady aerodynamics: Subsonic compressible inviscid case. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
8

Sarkar, Sutanu. Compressible homogeneous shear: simulation and modeling. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1992.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
9

Erlebacher, Gordon. The analysis and simulation of compressible turbulence. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
10

Roe, P. L. Error estimates for cell-vertex solutions of the compressible Euler equations. Hampton, Va: ICASE, 1987.

Find full text
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Compressible flow"

1

Rennels, Donald C., and Hobart M. Hudson. "Compressible Flow." In Pipe Flow, 31–47. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118275276.ch4.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Ferziger, Joel H., Milovan Perić, and Robert L. Street. "Compressible Flow." In Computational Methods for Fluid Dynamics, 421–45. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-99693-6_11.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Canuto, Claudio, M. Yousuff Hussaini, Alfio Quarteroni, and Thomas A. Zang. "Compressible Flow." In Spectral Methods in Fluid Dynamics, 240–74. Berlin, Heidelberg: Springer Berlin Heidelberg, 1988. http://dx.doi.org/10.1007/978-3-642-84108-8_8.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Ferziger, Joel H., and Milovan Perić. "Compressible Flow." In Computational Methods for Fluid Dynamics, 291–310. Berlin, Heidelberg: Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/978-3-642-98037-4_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Sherwin, Keith, and Michael Horsley. "Compressible flow." In Thermofluids, 512–38. Boston, MA: Springer US, 1996. http://dx.doi.org/10.1007/978-1-4899-4433-7_25.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Zohuri, Bahman, and Nima Fathi. "Compressible Flow." In Thermal-Hydraulic Analysis of Nuclear Reactors, 231–52. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17434-1_7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Ferziger, Joel H., and Milovan Perić. "Compressible Flow." In Computational Methods for Fluid Dynamics, 309–28. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-642-56026-2_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Sherwin, Keith, and Michael Horsley. "Compressible flow." In Thermofluids, 103–7. Boston, MA: Springer US, 1996. http://dx.doi.org/10.1007/978-1-4899-6870-8_25.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Zohuri, Bahman. "Compressible Flow." In Thermal-Hydraulic Analysis of Nuclear Reactors, 279–305. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-53829-7_7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Ferziger, Joel H., and Milovan Perić. "Compressible Flow." In Computational Methods for Fluid Dynamics, 283–301. Berlin, Heidelberg: Springer Berlin Heidelberg, 1996. http://dx.doi.org/10.1007/978-3-642-97651-3_10.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Compressible flow"

1

Sarkar, Sutanu. "COMPRESSIBLE TURBULENCE." In Fifth International Symposium on Turbulence and Shear Flow Phenomena. Connecticut: Begellhouse, 2007. http://dx.doi.org/10.1615/tsfp5.20.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Mirshekari, Gholamreza, and Martin Brouillette. "Compressible Microchannel Flow." In ASME 2010 8th International Conference on Nanochannels, Microchannels, and Minichannels collocated with 3rd Joint US-European Fluids Engineering Summer Meeting. ASMEDC, 2010. http://dx.doi.org/10.1115/fedsm-icnmm2010-30399.

Full text
Abstract:
We present experiments on the isothermal gas flow at relatively high Mach numbers in microfabricated channels of small aspect ratios. The microchannels were fabricated by deep etching on silicon wafers, bonded to a Pyrex wafer to cover and seal them; the microchannels were 10 microns deep with a variety of widths. The accurate determination of the small flow rates was performed by measuring the displacement of a bead of mercury in a precision bore glass tube in a controlled environment. The experiment setup has been specially designed to account for inlet and outlet loss. The inferred friction coefficient at different values of Knudsen, Reynolds and Mach numbers shows that the flow inside the microchannel follows the classical laminar behavior over the range of experiments.
APA, Harvard, Vancouver, ISO, and other styles
3

Patil, Sunil, and Terry Ng. "Compressible Wake Stabilization Using Periodic Porosity." In 5th Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4834.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Ali, T. Ait, S. Khelladi, L. Ramirez, and X. Nogueira. "Cavitation modeling using compressible Navier–Stokes and Korteweg equations." In MULTIPHASE FLOW 2015. Southampton, UK: WIT Press, 2015. http://dx.doi.org/10.2495/mpf150361.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

YU, KEN, EFFIE GUTMARK, and KLAUS SCHADOW. "Passive control of coherent vortices in compressible mixing layers." In 3rd Shear Flow Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3262.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

LIN, BING-QIU. "The shearing and convecting motion of the compressible vortex." In 2nd Shear Flow Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-996.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

EBERHARDT, S., and D. BAGANOFF. "Overset grids in compressible flow." In 7th Computational Physics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1524.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Majdalani, Joseph. "The Compressible Taylor-Culick Flow." In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-3542.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Arlitt, Raphael G. H., Martin Oberlack, and Norbert Peters. "COMPRESSIBLE TURBULENT FLOW: SYMMETRIES AND SCALING LAWS." In First Symposium on Turbulence and Shear Flow Phenomena. Connecticut: Begellhouse, 1999. http://dx.doi.org/10.1615/tsfp1.1750.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Lagha, Maher, John Kim, Jeff Eldredge, and Xiaolin Zhong. "TURBULENCE PHYSICS OF COMPRESSIBLE BOUNDARY LAYERS." In Seventh International Symposium on Turbulence and Shear Flow Phenomena. Connecticut: Begellhouse, 2011. http://dx.doi.org/10.1615/tsfp7.940.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Reports on the topic "Compressible flow"

1

Berger, Marsha. Adaptive Methods for Compressible Flow. Fort Belvoir, VA: Defense Technical Information Center, March 1994. http://dx.doi.org/10.21236/ada277861.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Walker, J. D. Shear Layer Breakdown in Compressible Flow. Fort Belvoir, VA: Defense Technical Information Center, November 1995. http://dx.doi.org/10.21236/ada303627.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

STRICKLAND, JAMES H. Gridless Compressible Flow: A White Paper. Office of Scientific and Technical Information (OSTI), February 2001. http://dx.doi.org/10.2172/780296.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Kerschen, Edward J. Receptivity Theory in Compressible Jet Flow Control. Fort Belvoir, VA: Defense Technical Information Center, March 1997. http://dx.doi.org/10.21236/ada325563.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Bisek, Nicholas J. High-Fidelity Numerical Modeling of Compressible Flow. Fort Belvoir, VA: Defense Technical Information Center, November 2015. http://dx.doi.org/10.21236/ada625106.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Tezaur, Irina Kalashnikova, Jeffrey A. Fike, Kevin Thomas Carlberg, Matthew F. Barone, Danielle Maddix, Erin E. Mussoni, and Maciej Balajewicz. Advanced Fluid Reduced Order Models for Compressible Flow. Office of Scientific and Technical Information (OSTI), September 2017. http://dx.doi.org/10.2172/1395816.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Poggie, Jonathan. Numerical Modeling of Compressible Flow and Its Control. Fort Belvoir, VA: Defense Technical Information Center, March 2014. http://dx.doi.org/10.21236/ada599340.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Liu, Wing K. Multiresolution Analysis of Compressible Viscous Flow-Structure Interaction. Fort Belvoir, VA: Defense Technical Information Center, March 2000. http://dx.doi.org/10.21236/ada377739.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Chenoweth, D. R., and S. Paolucci. Compressible flow of a multiphase fluid between two vessels:. Office of Scientific and Technical Information (OSTI), June 1990. http://dx.doi.org/10.2172/6490422.

Full text
APA, Harvard, Vancouver, ISO, and other styles
10

Suo-Anttila, A. F2D users manual: A two-dimensional compressible gas flow code. Office of Scientific and Technical Information (OSTI), August 1993. http://dx.doi.org/10.2172/10188561.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Compressible flow' for particular source types:
Journal articles Dissertations / Theses Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography