National Transonic Facility

From NasaCRgis

(Redirected from 1236)
Jump to: navigation, search
Building 1236
Building exterior

Center: Langley Research Center
Location: Hampton, Virginia
Year Built: 1947
Historic Eligibility: National Register Eligible
Important Tests: Boeing 777, Space Shuttle, Boeing 767, B-2 Bomber, A-6 Intruder, F-18 Hornet

Back Arrow.jpg Property Index


[top] History

The site of the National Transonic Facility (NTF) was originally the site of Langley's first large supersonic wind tunnel. The 4 x 4-Foot Supersonic Pressure Tunnel was a hurried necessity and designing began February 1945 with completion scheduled by the end of 1945. NACA launched the project of building a Mach 2 tunnel within 10 months. Contractors were hired for the mechanical design and actual fabrication of the tunnel. Near the end of 1945, the objective was near completion but a 2-year strike halted production of the compressor and operation didn’t begin until 1948.

Many important military and space vehicle tests were conducted in the 4 X 4-Foot Supersonic Pressure Tunnel. Century Series fighters like the F-102 and F-105, the B-58 supersonic bomber, and the X-2 research aircraft were all tested here. It was such an asset to NACA that it underwent modifications in 1950 for new drive motors which increased the horsepower from 6,000 to 45,000 (continuous) and 60,000 (intermittent). During the early 1970's, operation of the 4 X 4 Supersonic Pressure Tunnel was transferred to the 16-Foot Transonic Tunnel staff. During this period the facility was used for performance tests on military aircraft such as the F-14 and F-15 (See It's yours. No, it's yours.) and for general research on nozzle performance and propulsion airframe integration. The last research run in the facility was conducted on a Single-Engine High-Pressure Air Nacelle Model on September 2, 1976 and the "official" tunnel retirement date was September 3, 1976. The tunnel was decommissioned in 1977, as plans for NTF were conceived. Parts of the 4 X 4 were integrated into NTF’s design like drive motors, cooling towers, and surrounding support facilities.

The need for the large transonic tunnel was accepted nationally during the 1960s. The acceptance came after breakthroughs were made with the 0.3 meter transonic cryogenic tunnel at Langley. Many plans and alternatives were made but all of them were terminated due to extremely high costs. NASA's recent successes with cryogenics backed a proposal for a 2.5 meter cryogenic transonic tunnel. The U.S. Air Force wanted an intermittent high-pressure Ludweig-tube tunnel for transonic test requirements. Both of these facilities would have been expensive to build so it prompted the federal government to combine the projects and build one National Transonic Facility. The approximate cost was $85 million but it would serve to fulfill all U.S. commercial, military, and scientific requirements. Completion date was set for 1982 and the first ton of cryogenic nitrogen flowed through NTF in 1983.

NTF is high-pressure, cryogenic, and closed circuit. Super-cold nitrogen gas is used in the test section at high pressure to simulate true flight aerodynamics. The facility has a drive power of 135,000 hp and reaches Mach 1.2 speeds. What makes NTF unique is it can test models from one-fifteenth scale to full because it can adjust the airflow according to the model size unlike traditional wind tunnels. NTF has provided the highest quality of flight Reynolds number aeronautical data to the research, industry, and Department of Defense communities. Noteworthy tests in NTF include the Boeing 777, the Space Shuttle and Booster, the Boeing 767, the B-2 Bomber, the A-6 Intruder, and the F-18 Hornet.

Today, NTF at Langley is used for tests in cruise performance, configuration aerodynamics validation, support of stability and control, and stall buffet onset. What also makes NTF unique is that it has a 150 cubic foot space vacuum used for testing. The vacuum was completed in 1965. NTF also has its own liquid nitrogen plant to supply the facility with the nitrogen gas needed for testing. Groundbreaking for the plant was in October of 2007 and the plant is fully operational today.

[top] Photos

[top] Facility

1968 Exterior Prior to Rehab as NTF1978 Artist's Rendering19781980NTF Facility Photos

[top] Personnel and Awards

1984 Group Achievement Award1984 Group Achievement Award1990 Group Achievement Award

[top] Posters


[top] Models

See 4X4 Tunnel Models for tests conducted prior to change to NTF

1985 EA-6B ModelPathfinderPathfinder1985 Pathfinder in NTF1985 Space Shuttle Model1985 Shuttle Ascent1985 Shuttle Orbiter Model1985 Shuttle Orbiter Model1986 Submarine1990 High Speed Civil Transport Model1992 Cessna Citation1993 USAF C-171996 NTF Semispan Model1999 NTF Q-probe Check Standard1999 Q-probe Check2000 777 Semi-span Model2001 Boeing 777 Test 119

[top] Films

1995 NASA Astronaut Visit

1990 Pathfinder Strut Test J-491

[top] Interviews

Bill Conkling on Fabrication of NTF Blades

[top] Documents

1977 Dedication Program

Building Brochure

1978 Transonic Tunnel Chronology Relevant to NTF

1978 Chronology of NTF Related Events

1983 Special Issue of Langley Researcher on NTF

1983 NTF dedication program with George Bush

1986 Modifications to Facility

Employment opportunities at NTF as result of shakedown

1989 Newspaper Article on Tunnel's Closure because of Damage

1989 Modifications to NTF for Independent Operation

1990 Facility Resume

1990 Proposal for National Resource Protection

1989 Modifications to NTF for Independent Operation

1997 Facility Details on NTF

2006 Industry Uses NASA Wind Tunnels to Design New Airplane

2007 Ceremony Break Ground (new liquid nitrogen plant)

2007 Facility Overview

2009 Orion Testing in World Class Facility

Brochure on NTF

Relative Location of Proposed Storage Tank

Personal tools