Technological advancement, particularly in aeronautics, is
not easy. This fall, as we remembered
the passing of President Kennedy, his speech proposing the landing of Americans
on the moon was played often. "We choose to go to the
moon in this decade and to do these other things not because they are easy, but
because they are hard, because that goal will serve to organize and measure the
best of our energies and skills,…”
This
fall also marks the 60th anniversary of the introduction of the
F-100 Super Sabre into the United States Air Force. Like the Boeing 787
Dreamliner, the F-100 pushed the boundaries of conventional technology. The F-100 Super Sabre was the first
operational aircraft to be designed for and capable of supersonic speed in
level flight. The pioneering technology
necessary to accomplish this, from aerodynamics to propulsion, was no less
dramatic than that of the Dreamliner.
Unlike
the Boeing 787, propulsion requirements for the F-100 to achieve its intended
supersonic capability could not be satisfied by current turbojet technology. Therefore, a new turbojet engine design was
needed. The progeny of that effort was
the Pratt and Whitney J-57 (JT-3). The engine design was so revolutionary that the 1952 Collier Trophy was awarded for the J57. Fitted with recently developed
afterburner technology, the J57 met the expectations for the F-100 design
objectives. That engine proved to be
integral to the success of not only the F-100, but other famous aircraft as
well. The legacy of many iconic
airplanes like the F-101, F-102, U-2, F-8, B-52, B-57, Boeing 707 and Douglas
DC-8 was created in no small part because of the J57.
North
American Aviation Chief Test Pilot, George Welch (pictured above), flew the first production
F-100A on October 29,1953. On a second
flight that day, USAF test pilot Lt. Col “Pete” Everest Jr. set a world speed
record of 755.149 over the Southern California desert near the Salton Sea. This was the last speed record established at
low altitude. Welch had also flown the YF-100A prototype the previous May 25 on
its maiden flight that included speeds above Mach 1.0. Welch was no stranger to either first or
supersonic flights. He piloted the North American Aviation F-86 on its first flight October 1, 1947. Also, although not
officially recorded and in a dive, Welch exceeded the Mach 1 in an F-86 just
days before Chuck Yeager exceeded the sound barrier in level flight in his “Glamorous Glennis”
Bell X-1A.
Welch’s career is less widely known than Yeager’s, but his
story is equally interesting. On the
morning of Sunday December 7, 1941, after an all night party, Lt’s George Welch
and Kenneth Taylor were intending on going for a swim at their auxiliary base
Haleiwa Field about 10 miles from the Wheeler Field at Pearl Harbor when the Japanese
attack began. On their own initiative
the pilots drove to the aux field where Welch had called ahead to have two
P-40s readied for takeoff. The two
pilots took off without orders and engaged the attackers. Their actions are highlighted in many war
movies about Pearl Harbor, including the 1970 film, Tora Tora Tora. Welch recorded 4 kills that day and, as well
as Taylor, received the Distinguished Flying Cross for his heroism.
Unfortunately, George Welch lost his life October 12, 1954 on
a test flight of the F-100. While
performing one of the final evaluations of the Super Sabre’s design, a maximum
load high-speed pull up maneuver, the aircraft became uncontrollable and was
lost. The 36-year-old Welch was able to
eject, however, the injuries he sustained in the accident were fatal. Stability
issues were reported by all of the pilots that had test flown the F-100A. Most troublesome were poor longitudinal
stability in high-speed flight as well as poor low-speed handling
characteristics. The low-speed qualities
of the F-100 would prove to be fatal for many pilots who failed to acknowledge
it’s unique handling characteristics.
The high-speed instability would be solved, but would require all new
high speed jet fighters to respect a phenomenon that cost George Welch his
life, inertial roll coupling.
Prior to the F-100, fighter aircraft were neither heavy nor
fast enough to experience inertial coupling.
Inertial coupling, simply explained is where the inertia of a longer
heavier fuselage overpowers the aerodynamic forces of the wings and tail. It
became problematic with the introduction of the supersonic F-100 with its long heavy
fuselage versus its relatively narrow wingspan. The inertial coupling problems were eventually
overcome, but not before six fatal crashes and a grounding of the aircraft in
October of 1954. Modifications to the F-100 were made
that included increasing the size of the vertical tail, adding a yaw dampener
as well as increasing the wingspan. The low speed characteristics of the F-100 remained
troublesome for its entire history.
Although the F-100's low speed performance benefitted greatly from the aerodynamically controlled slats introduced on the F 86, they allowed for higher angles of attack that also had distinct disadvantages. Also, the F-100 had large conventional ailerons that were responsible for the Super Sabre’s legendary adverse yaw. When the aircraft was turned the aileron on the “up wing” or the outside of the turn would deflect downward into the relative wind. This aileron’s deflection would create drag and induce a yawing motion away from the turn. This tendency was greatly exaggerated at low airspeed with high angles of attack. If the yawing were not corrected with rudder, the plane would eventually roll over in the opposite direction of the turn. If this happened in the landing pattern or close to the ground both the pane and pilot were often lost.
Also, through the use of the aircraft's automatic slats the F-100 was
capable of a very tight turning radius that was useful in air-to-air combat. This
ability to achieve high angles of attack also had disadvantages. The airplane’s unique aerodynamic
characteristics caused the airplane to experience large amounts of induced drag
from the F-100s wings. The 45-degree
wing sweep also contributed the center of lift to moving forward at high angles
of attack and causing a pitch up. During
air combat maneuvers this pitch up would cause the airplane to slow dramatically
and lose energy quickly. The J57 did not
have enough thrust to overcome this substantial induced drag. Although the F-100 could turn tighter than its opponent, the energy deficit would leave the pilot vulnerable
to a faster enemy plane. Even more
pernicious were the consequences from the enormous induced drag in the landing
pattern or maneuvering close to the ground.
The F-100 wing could fly without stalling at a speed low enough to
create more drag than the J57 could overcome.
This flight regime is described as the area of reverse command. Pilots
refer to it as being “behind the power curve”.
It is the condition of the aircraft filmed doing the infamous “Sabre
Dance”. The engine could not provide
enough thrust, even in afterburner, to overcome the induced drag and allow the
pilot to “fly” out of his situation.
Numerous models of the F-100 Super Sabre were flown by the air forces of Turkey, France, Denmark and Taiwan. Air National Guard pilots flew the last USAF F-100 operational sortie in November 1979. During the 25 years the F-100 Super Sabre was in the USAF inventory, all who flew it, including the USAF Thunderbirds, admired as well as respected this remarkable airplane. I feel very lucky to be in a small group of pilots that have had the priveldge to fly both the Super Sabre and the Dreamliner.
“You’ve got to pay your dues if you want to sing the blues
‘Cause you know it don’t come easy”
Richard
Starkey
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