Two Dimensional Wind Tunnel

Code: LBNY-0005-1620001

The test section can be fitted with two interchangeable variable incidence model carriers, one with a cylindrical section and the other with a low velocity sub-sonic aerofoil. The cylinder has a single static tapping whi…

Two Component Balance

Code: LBNY-0005-1620002

Adjustable balance weights allow easy initial setup and zeroing of the system. Two component balance features a simple unique lever system employing vertical and horizontal balance beams to provide independent measuremen…

Pressure Cylinder

Code: LBNY-0005-1620003

Mounts vertically and spans the test section of an Educational Wind Tunnel Angular position is adjustable Comes with ample tubing 24 flush-mounted pressure taps around its circumference Outside diameter of 4 inches (…

Water Tunnels And Channels

Code: LBNY-0005-1620004

Top Speed: Demonstrated - 60 ft/sec (18.3 m/s) Nominally - 30 ft/sec (9.1 m/s)…

Model Positioning System

Code: LBNY-0005-1620005

Trans/supersonic systems: Nominal pitch angle range: <10 degrees + / <5 degrees. Subsonic systems: Nominal yaw angle range: +/- 30 degrees typical Nominal pitch angle range: +/- 30 degrees typical…

Yaw Probe

Code: LBNY-0005-1620006

Featured machined aluminum triangle that shows the orientation of the ports from outside the test Section and acts as a handle Three ports Mounts easily in the test section of an Educational Wind Tunnel Length of 10.5…

Traverse Systems

Code: LBNY-0005-1620007

Sweep area - based on each unique test section and application Position accuracy - customer defined. Optional Features: Models and Probes Data Acquisition and Control (DAC) System.…

Pressure Wing

Code: LBNY-0005-1620008

18 Flush-mounted pressure taps around its Clark Y-14 airfoil Angular position is adjustable Mounts vertically and spans the test section of an Educational Wind Tunnel (12 inches / 30.48cm) Comes with ample tubing Pre…

Pitot Static Probe

Code: LBNY-0005-1620009

Features a rounded-tip total-pressure tap Reaches 2.6 inches (6.6cm) forward of the bend Has an OD of 0.125 inches (3.175mm) 6 static ports Extends 13 inches (33cm) to the bend Comes with ample tubing.…

Flat Plate And Mouse

Code: LBNY-0005-16200010

Demonstrate and study boundary layers and boundary layer growth with ease. The pressure probes ascend on an angle covering a width of one inch (25.4mm) and a height of 0.24 inches (6.1mm). The probes are approximately 0.…

Flow Visualisation Wind Tunnel

Code: LBNY-0005-16200011

Ideal for small group experiments or classroom demonstrations, the apparatus is floor standing. A variablespeed fan mounted on top of the wind tunnel produces the air flow through the working section. Air flow is vertica…

Pyramidal Balance

Code: LBNY-0005-16200012

Pyramidal Balance can be divided into two main groups: internal and external. The group names are derived from their location relative to the test model and wind tunnel test section internal balances reside inside a test…

Sting Balance

Code: LBNY-0005-16200013

Balances can be divided into two main groups: internal and external. The group names are derived from their location relative to the test model and wind tunnel test section internal balances reside inside a test model, w…

Educational Wind Tunnel

Code: LBNY-0005-16200014

The Complete Educational Wind Tunnel System is an easy-to-use, all-in-one fluids aerodynamics laboratory. Optional features include instrumentation, data acquisition, models and probes. Educational Wind Tunnel (EWT) Syst…

Schlieren Systems

Code: LBNY-0005-16200015

In supersonic flow, air experiences very large changes in density as it approaches, passes through and trails shock waves. As the density of air changes, so does its index of refraction. Schlieren Systems let you see sho…

Closed Circuit Wind Tunnels

Code: LBNY-0005-16200016

Most Closed Circuit Wind Tunnels designs are traditional single-return, horizontally arranged circuits. However, any configuration is possible. As with all wind tunnels, exceptionally steady test section flow with close …

Blow Down Wind Tunnels

Code: LBNY-0005-16200017

Blow Down Wind Tunnels are a special type of Open Circuit wind tunnel. For Blow Down Wind Tunnels, however, air is blown down into the wind tunnel by a fan located upstream of the test section, as the name implies. Compa…

Transonic Wind Tunnels

Code: LBNY-0005-16200018

Employing variable test section porosity, computer-controlled valves, chokes and flaps, target airspeeds are easy to achieve and maintain. Using compressed air Transonic Wind Tunnels offer running speeds of M=0.3 to M=1.…

Supersonic Wind Tunnel

Code: LBNY-0005-16200019

Supersonic flow and the occurring shock waves can be directly observed with the supplied Schlieren optic apparatus. The continuous operation can allow enough time to take measurements and to observe the phenomena. This a…

Fan Test Stand

Code: LBNY-0005-16200020

The centrifugal fan which has a low chord impeller and split volute diffuser casing is directly driven by a DC dynamometer giving a variable speed from 0-4000 rpm, with a swinging stator providing load cell torque measur…

Boundary Layer Experiment

Code: LBNY-0005-16200021

Boundary layer studies involve the determination of the thickness of this layer and the velocity profile within it. These parameters will vary with velocity of the fluid flowing over the surface, the distance from the le…

Subsonic Open Circuit Wind Tunnel

Code: LBNY-0005-16200022

Air enters the test section through a carefully designed contraction followed by an aluminum honeycomb flow straightener designed to ensure that the flow is steady in both magnitude and direction and has a flat transvers…

Turbulent Jet

Code: LBNY-0005-16200023

The apparatus is shown mounted on the working surface of the basic Air Flow Bench and connected to the blown experiment duct of the fan by a re-enforced plastic hose. The equipment consists of a plenum chamber with outle…

Wind Tunnel Lab