XF-84H Thunderscreech

From Wikipedia, the free encyclopedia

XF-84H Thunderscreech
USAF XF-84H Thunderscreech
Type fighter
Manufacturer Republic Aviation Company
Maiden flight July 22, 1955
Primary users Republic Aviation Company
United States Air Force
Number built 2
Developed from F-84F Thunderstreak

The Republic Aviation Company XF-84H Thunderscreech was an experimental American-built turboprop aircraft based on the the F-84F Thunderstreak. Its turbine engine drove the plane with a supersonic propeller as well as its exhaust. Although only one ever flew, it set the unofficial air speed record for propeller-driven craft.

It was originally unofficially designated XF-106, while it was being developed for the US Navy [1]. After the project was taken over by the USAF it was renamed to XF-84H.[citation needed]

Contents

[edit] Design and Development

The XF-84H was created by modifying F-84F Thunderstreak aircraft. The engine was changed to an Allison XT-40-A-1, capable of 5,850 horsepower. An afterburner was installed but never used, which could increase power to 7,230 hp.

The propeller was a square blade turning at a constant 3,000 rpm, with the tips travelling at approximately Mach 1.18. Thrust was adjusted by changing the blade pitch.

The tail was modified to a T-tail to avoid turbulent airflow flow over the horizontal stabilizer/elevator surfaces from propeller wash.[2]

The XF-84H was the first plane to carry a ram air turbine. In the event of failure of the engine, it would automatically swing out into the airstream to provide extra hydraulic and electrical power.

[edit] Testing

The Thunderscreech was destabilized by the powerful torque from the propeller, as well as inherent problems with supersonic propeller blades. It was plagued with engine related problems that affected other aircraft of the time with similar Allison T40 engines such as the Douglas XA2D Skyshark and the North American A2J Super Savage attack aircraft.

It flew a total of 12 test flights. One test pilot flew in it once and refused to ever fly in it again.

Test pilot Hank Baird took the craft up eleven times and ten of these flights ended in forced landings.

It was possibly the loudest plane ever built, earning the nickname 'Thunderscreech'.[3] On the ground, they were reportedly audible 25 miles away. Ground crew reported that nearby, standard ear protectors "made no difference".

[edit] The Noise

The propeller blades were supersonic even while the airplane was running up on the ground. Each blade shed a shock wave that spiraled outward. It was more than just sound. Sound is a series of smooth waves of variable frequency and amplitude. Shock waves change the nature of the air carrying them, a fundamental difference from sound waves. They are typified by a nearly instantaneous pressure increase, which causes an impact upon reaching a solid surface.

A person standing some distance from the airplane was subjected to rapid fire shock waves. The shock waves acted on the body, causing spasms, nausea, and loosening of the bowels. Even epileptic fits were reported. Ear protection made no difference.

In short order, the Air Force Flight Test Center directed Republic to tow the XF-84H out on Rogers Dry Lake, far from the flightline, before running up its engine.

[edit] Historical significance

It holds the record in the Guinness Book of Records as the fastest propellor driven plane ever built,[4] with a design top speed of 670 mph (Mach 0.9), it is reported to have reached 623 mph (Mach 0.83).

It was only ever flown by the Republic test pilots, making it possibly the only USAF plane to be never flown by a USAF pilot.

[edit] Surviving plane

Two prototypes were built (FS-059 and FS-060) and only the FS-059 ever flew, logging only 10 hours.

FS-059 (pictured) was retired and spent many years mounted on a pole outside Meadows Field Airport, Bakersfield, California. It was taken to the 178th Fighter Wing of the Ohio Air National Guard whose volunteers spent over 3,000 hours bringing the Thunderscreech back into display condition. It is now on show at the National Museum of the United States Air Force at Wright-Patterson Air Force Base near Dayton, Ohio.

FS-060 (currently unknown). Assumed scrapped when the project was decommissioned in 1956, along with the plans.

[edit] Specifications

General characteristics

  • Crew: 1
  • Length: 51 ft 5 in (15.67 m)
  • Wingspan: 33 ft 5 in (10.18 m)
  • Height: (4.69 m)
  • Wing area: 30.75 m ()
  • Empty weight: 17,892 lb (8,132 kg)
  • Loaded weight: 27,046 lb (12,293 kg)
  • Max takeoff weight: lb (kg)
  • Powerplant: × , () each

Performance

Armament

3 x g16mm

[edit] References

  1. ^ http://www.designation-systems.net/usmilav/duplications.html
  2. ^ http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=2296
  3. ^ Knaack, Marcelle Size. Encyclopedia of US Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters 1945–1973. Washington, D.C.: Office of Air Force History, 1978. ISBN 0-912799-59-5.
  4. ^ The Guinness Book of Records 1997, page 137; ISBN 0-85112-014-8.
  • Bowers, PM, Angellucci, E. The American Fighter. New York: Orion Books, 1987. ISBN 0-517-56588-9.

[edit] External links

[edit] Related content

Wikimedia Commons has media related to:

Related development

Comparable aircraft

Designation sequence

Related lists

See also