Low Speed Wind Tunnel Testing Barlow Pdf Editor

14.09.2019
Low Speed Wind Tunnel Testing Barlow Pdf Editor 4,1/5 1487 reviews

A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. The High Speed Wind Tunnel is a blowdown-to-atmosphere, transonic-supersonic, adjustable-Mach-number facility. The general arrangement of the facility is shown in an aerial photograph in Figure 2-1. A schematic drawing indicating wind tunnel circuit layout is provided as Figure 2-2. Figure 2-1 High Speed Wind Tunnel General Arrangement.

Barlow, Jewel

Low Speed Wind Tunnel Design

Director of Glenn L. Martin Wind Tunnel
Associate Professor Emeritus
2102 Martin Wind Tunnel

EDUCATION

  • B.S., Auburn University Engineering (Physics)
  • M.S., Auburn University (Aerospace Engineering)
  • Ph.D., University of Toronto (Aerospace Engineering)

PROFESSIONAL MEMBERSHIPS

Member of SAE Road Vehicle Aerodynamics Committee

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Research in applied aerodynamics, experimental aerodynamics, flight mechanics and control, and the vehicle design process.

Books

  • Low Speed Wind Tunnel Testing, 3rd Edition, John Wiley & Sons, Inc., 1999

Journal Articles

  • Barlow, J.B., Guterres, R., and Ranzenbach, R., “Experimental Parametric Study of Rectangular Bodies with Radiused Edges in ground effect”, Journal of Wind Engineering and Industrial Aerodynamics, Volume 89, Dec. 2001, pp. 1291-1309.
Editor

Conference Proceedings

  • Ro, K., and Barlow, J. B., “Dynamic Modeling of Articulated Wing-Body-Tail Aerial Vehicles”, AIAA-2005-1024, 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan 2005
  • Bryant, E., Owens, D., and Barlow, J.B., “Free-to-Roll Investigation of Uncommanded Lateral Motions for an Aircraft with Vented Strakes”, AIAA 2005-239, 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan 2005
  • Cook, S., and Barlow, J., “Investigation of Flow Topology and Aerodynamic Bifurcation for Aircraft with Vented Strakes”, AIAA-2004-2154, 34th AIAA Fluid Dynamics Conference and Exhibit, Portland, OR June 2004
  • Cook, S. and Barlow, J., “An Investigation of Low-Speed Lateral Characteristics of a Simplified F/A-18E Configuration”, AIAA paper 2003-931, 41st Aerospace Sciences Meeting, Reno, NV, Jan. 2003.
  • Cook, S. and Barlow, J., “Investigation of Critical States of the F/A-18E in Power Approach Configuration Using Mini-Tuft Flow Visualization”, AIAA-2001-4145, AIAA Atmospheric Flight Mechanics Conference, August 6-9, 2001, Montreal, Quebec, Canada.
  • Ranzenbach, R., Barlow, J., and Esmaili, H., “Practical Application of the Two-Variable Blockage Correction Method to Automobile Shapes', SAE paper 2001-01-0632 in Vehicle Aerodynamics Design and Technology, SAE SP-1600, SAE 2001 World Congress, Detroit, MI, March 2001.
  • Barlow, J.B., Guterres, R.G., and Ranzenbach, R.R., “Parametric Study of Wake Structures and Forces of Rectangular Bodies with Radiused Edges Near a Plane Surface”, SAE 2000-01-0490 in SP-1524, SAE Congress, Detroit, MI, February, 2000
  • Barlow, J., Guterres, R., and Ranzenbach, R., “Experimental Parametric Study of Rectangular Bodies with Radiused Edges in Ground Effect”, in proceedings of 4th International Colloquium on Bluff Body Aerodynamics and Applications, Ruhr Universistat Bochum, Germany, September 11-14, 2000.
  • Barlow, J., Guterres, R., and Ranzenbach, R., “Rectangular Bodies with Radiused Edges in Ground Effects”, AIAA paper 00-4014, in proceedings of 18th AIAA Applied Aerodynamics Conference, Denver, CO, August 14-17, 2000.
  • Cook, S. and Barlow, J., “Investigation of Effects of Leading Edge Extension Vents on the Lateral Characteristics of the F/A 18-E/F in Power Approach Configuration”, AIAA-2000-4510, in proceedings of 18th AIAA Applied Aerodynamics Conference, Denver, CO, August 14-17, 2000.
  • Barlow, J.B., Guterres, RG., and Williams, J., 'Wake Structures of Rectangular Bodies with Radiused Edges Near a Plane Surface', SAE paper 1999-01-0648 in SAE SP-1441, SAE Congress, Detroit, MI, February, 1999
  • Williams, J., Barlow, J.B., and Ranzenbach, R, 'Experimental Study of Cd Variation with Vehicle Aspect Ratio', SAE paper 1999-01-0649 in SAE SP-1441, SAE Congress, Detroit, MI, February, 1999

Glenn L. Martin Wind Tunnel Featured in the News

Reporters from national and regional television networks experienced hurricane-force winds firsthand.

Students Shine at AIAA Region 1 Student Conference

Twelve students won awards for their papers, and seven were from UMD.

Researchers Demonstrate New Approach to using PIV in the Glenn L. Martin Wind Tunnel

UMD Researchers Demonstrate Successful Use of PIV for Time-resolved Flow Field Measurements

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University of Maryland offers reporters the chance to experience hurricane-force winds firsthand.

National Media Highlights UMD Hurricane Research, Wind Tunnel

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15 Department of Aerospace Engineering's faculty honored for successful research funding efforts.

University of Maryland Wind Tunnel Featured in Motorweek

UMD staff helps test aerodynamic efficiency of Genovation’s green G2 car.

Glenn L. Martin Wind Tunnel Gets a New Coat..of Paint

GLMWT Laboratory Gets A Fresh Paint Job

Kothari hosts 30th Graduation Anniversary dinner

Kothari hosts 30th Graduation Anniversary dinner at home

Wind Tunnel Testing Pdf

Leishman named 2007 AHS Technical Fellow

Dr. Leishman is one of the leading experts in rotorcraft aerodynamics

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