Capabilities
Operating Characteristics
Test Section Dimensions
Model Installation Diagram
Forward and Aft Limits
Forces and Moments
Load Compensation
Turntable Model Support
Semispan Testing
Installation and Personnel Access
Flow Visualization
High-Pressure Air

 11-by 11-foot Transonic Wind Tunnel

LB435 Model in 11 Foot Test Section 

Capability

 

Mach Number: 0.20 to 1.45

Rn = 0.30 to 9.6 million per foot

Stagnation Pressure, PSIA: 3.0 to 32.0

Maximum stagnation temperature = 150°F. Typical Temperature variation over the course of a test = 20°F

Closed circuit, single return, variable density, continuous flow wind tunnel

Interchangeability of models between Unitary test sections allows testing across a wide range of conditions

Internal strain-gage sting mount, model component and floor balances are used for measuring forces and moments. Ames and Langley inventories typically available

Full support of DTC PSI module capability

Support strut has simultaneously variable pitch and yaw capability (plus or minus 15°)

There are two controllable 3000 psi auxiliary air systems capable of flow rates up to 40 lb/sec each. One line can be controlled up to 80 degrees F and the other up to 400 degrees F

User interaction will be X-terminal based

Full internal and external network capability. PCs and Macs available to customers as needed

Typical two weeks of model build up and instrument preparation is included in the facility occupancy charge

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Operating Characteristics

 

 
11ft Transonic Wind Tunnel Operating Characteristics
The operating characteristics of the 11ft Transonic Wind Tunnel are presented in the graph to the left.

 

* Click on image to enlarge

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Test Section Dimensions

 

Pertinent Test Section Dimensions are:
Height
11.0 ft.
Width
11.0 ft.
Length
22.0 ft.
Access hatch, top:
7.0 x 22.0 ft.
Side doors:
3.0 x 4.9 ft.

11ft Transonic Wind Tunnel Test Section Drawings
Plan View

Drawing Plan View Pic
* Click on image to enlarge

Auto CAD Files:

DWG Icon

11ftTSplan.dwg

Version 2000i AutoCAD File

Translation Files:
 

DXF Icon

11ftTSplan_v2k.dxf

Version 2000
Drawing Exchange File

IGES Icon

11ftTSplan.igs

Initial Graphics Exchange Specification File

*
Note: Right Click (PC) / Control Click (Mac) and "Save As..." to Download Files. To Open, use "Import" function in drawing program.

Get Volo View Express: (Windows OS Only)

A free, downloadable application that lets you view and print basic design drawing formats.

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Elevation View

Drawing Elevation View Pic
* Click on image to enlarge

Auto CAD Files:

DWG Icon

11ftTSelev.dwg

Version 2000i AutoCAD File

Translation Files:
 

DXF Icon

11ftTSelev_v2k.dxf

Version 2000
Drawing Exchange File

IGES Icon

11ftTSelev.igs

Initial Graphics Exchange Specification File

*
Note: Right Click (PC) / Control Click (Mac) and "Save As..." to Download Files. To Open, use "Import" function in drawing program.

Get Volo View Express: (Windows OS Only)

A free, downloadable application that lets you view and print basic design drawing formats.

 

 

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Model Installation Diagram

 

11ft Transonic Wind Tunnel Sting Installation
This diagram shows a sting installed with a 40-inch extension.

 

* Click on image to enlarge

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Forward and Aft Limits

The forward and aft limits of the model location in the test section are dependent on the Mach number and the type of data required. As identified by tunnel station:

 
11 Foot Transonic Wind Tunnel Model Location Limits
Station
Limit
175
Aft limit for subsonic drag perfromance testing
193
Aft limit for subsonic static stability and control testing
220
Aft limit for supersonic static stability and control testing
60
Forward limit for subsonic testing
100
Forward limit for supersonic testing

*Consult the test manager for any deviations from these limits. 

 

 

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Forces and Moments

A traversing strut downstream of the test section can be programmed to translate vertically to maintain a desired point of model-pitch rotation throughout the vertical plane angle-range. The model support center-of-rotation in the horizontal plane is 4.8 inches aft of the strut leading edge. These angles are continuously variable and are determined by the relative positions of a knuckle and sleeve inside the support body.

The model support system can position the model at attitudes circumscribed by a 15-degree half-angle cone. Bent primary adapters of 5, 10, 12.5, and 20 degrees are available to alter the range of model angles. Forces and moments resolved at the model support center of rotation are limited to:

 
Vertical
± 8,000 lbs
Lateral
± 4,000 lbs
Axial
± 3,000 lbs
Rolling Moment
± 104,000 in-lbs
Combined Vertical and Lateral Bending Moment
± 800,000 in-lbs

NASA Ames Balance Inventory

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Load Compensation

A load compensation system capable of exerting a downward force of up to 8,000 lbs over a vertical travel range of 51 inches is available at tunnel stations 215.8 or 239.4. This system is used to offset high-lift forces which would otherwise exceed the design-load limits of the strut.

 

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Turntable Model Support

A subfloor-mounted turntable model support, used primarily for semispan model testing, is located at tunnel station 106. This support system can be rotated +180 degrees and forces and moments are limited to:

 
Lateral force (at a height of up to 24 inchest above the floor):
± 50,000 lbs
Torque (about axis of turntable):
± 500,000 in-lbs

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Semispan Testing

 

11 Foot Hatch Pic
Semispan model installed in 11 Foot Test Section

 

Provisions are available for sealing the slots in the test section floor to provide a solid image plane for semispan testing.

NASA Ames SemiSpan Balances and Load Ranges

EZ #

NEMS

INV #

Size / Model

NF
lbs

PM
in-lbs

AF
lbs

YM
in-lbs

RM
in-lbs

71

1809091

6K, MC-6.0-27.5

6000

3000

1200

6000

30000

69

1809090

15K, MC-150-27.5

15000

10000

3000

15016

75088

70

40K, MC-400-27.5

40000

20000

8000

40000

200000

 

 

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Installation and Personnel Access

11 Foot Hatch Pic
Hatch Dimensions: 7.0 ft. x 22.0 ft.
* Click on image to enlarge

 Models can be installed through a hatch in the top of the test section. Personnel gain access to the test section through doors in the diffuser sidewalls downstream of the model support strut.

 

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Flow Visualization

 Flow visualization techniques are available through multiple, optical-quality windows in the tunnel sidewalls. Optical-quality windows are also available in the test section ceiling and floor.

 

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High-Pressure Air

 High-pressure air (3,000 psi) is available at weight flows to 80 pounds per second through dual, independently regulated lines ending within the support strut. A one-megawatt, moveable heater can preheat air from one of these lines. Preheated air at 60 pounds per second is available at the turntable.

 

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