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Quest for Performance: The Evolution
of Modern Aircraft
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- Part I: THE AGE OF
PROPELLERS
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- Chapter 8: Boats in the Sky
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- Two Amphibian
Developments
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- [183] The
amphibian flying boat is a unique type of aircraft equally at home
operating from land or sea. Such aircraft trace their origins to
early experiments by Glenn H. Curtiss, but the type did not gain
popularity until the introduction of a highly innovative design
produced in 1924 by the Loening Aeronautical Corporation. The
Loening aircraft provided performance comparable to that of a
landplane of similar size and performance, the DH-4, but offered
the added capability of operation from either land or water. In an
era of few airports, this versatility, coupled with high
performance, was greatly appreciated. A photograph of a Loening
OA-1C amphibian is presented in figure 8.10, and pertinent
characteristics of the aircraft are given in table IV.
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- [184] The Loening
amphibian appears much as a conventional single-engine biplane but
with the lower part of the fuselage configured as a single-step
hull that extended forward of the engine and propeller. As can be
seen in figure 8.10, the wheels could be retracted into cavities
located on the sides of the hull for water operation. The entire
configuration concept was made feasible by an inverted V-12
Liberty or Packard engine that placed the thrust line sufficiently
high so that the propeller cleared the forward-projecting hull
without, at the same time, causing a fuselage of excessive
bulkiness. The two-bay biplane wing configuration was typical of
the time period but was unique in utilizing the N-type interplane
struts that eliminated much time-consuming effort in rigging the
wings. The tip-mounted lateral stabilizing floats also
incorporated skids to prevent damage in landplane
operations.
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- The hull was of wood-frame construction
covered with aluminum alloy sheets. Wooden spars and stamped
aluminum alloy ribs comprised the wing structure, which was
covered with fabric. Hand operation was required to retract the
landing gear in early models, but actuation by an electric motor
was provided in later versions. Open cockpits configured for two
or three occupants were usually provided.
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- A comparison of the physical and
performance characteristics of the OA-1C given in table IV with those of the DeHavilland DH-4 in table 1 indicates that the two aircraft are closely similar
in size, power, weight, and performance. The added versatility of
the Loening amphibian....
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- Figure 8. 10 - Loening 0A-1C
amphibian; 1924. [USAF via Martin
Copp]
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- [185]...assured it of
an important place in aeronautical activities in the 1920's and
1930's. Versions of the Loening amphibian were built not only by
Loening but, after the demise of that company, by Keystone and
even later by Grumman. The modernized version built by Grumman was
in production well into the World War II years. These latter
aircraft, designated Grumman JF and J2F were known as Ducks. All
later versions of the aircraft employed radial air-cooled engines
instead of the earlier water-cooled Liberty and Packard power
plants. All three services of the United States-Army, Navy, and
Coast Guard-as well as a number of civil operators utilized the
aircraft. A civil version having a single cockpit and
accommodations for four to six passengers in an enclosed cabin was
available in addition to the military models. Loening amphibians
participated in several record and exploratory flights that,
together with descriptions of the aircraft and its development,
are given in references 88 and 89.
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- Today, the name Igor Sikorsky is usually
associated with the pioneer development of the helicopter; but in
earlier years, he was known as the father of a number of
multiengine aircraft, including several excellent flying boats and
amphibians. One of these, the S-38 amphibian, first appeared in
1928 and established the great Russian designer in the United
States. Serving in a number of pioneer airline operations, notably
Pan American Airways, the aircraft was also used by various
military services and in several exploratory operations.
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- A side view of the S-38 is shown in figure
8.11. In configuration concept, the aircraft was reminiscent of
the NC boats described earlier and consisted of a short hull with
the tail assembly attached to outriggers extending from the upper
wing of the sesquiplane wing arrangement. Power was supplied by
two Pratt & Whitney nine-cylinder radial air-cooled engines
mounted side by side in nacelles located between the wings. A
large number of struts integrated the hull, wings, tail assembly,
and engines into a unified configuration. Lateral stabilizing
floats were located beneath the tips of the lower wings, and the
landing wheels retracted into the sides of the hull. A unique
feature of the landing gear was the capability for lowering the
wheels individually. One might question the advisability of such
an action, but turning moments were produced by the water drag of
one extended landing gear; thus steering capability, always a
problem while maneuvering on the water at low speeds, was
enhanced. Another interesting feature was incorporated in the
vertical tail surfaces that were cambered and laterally spaced so
that one surface was in the slipstream of each propeller. In the
event of the failure of one engine, the cambered surface in the
slip- stream....
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- [186] Figure 8. 11
Sikorshy S-38 10-passenger amphibian; 1928. [Joseph P. Juptner via AAHS]
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- ....of the other engine produced a yawing
moment opposite in direction to that caused by the power loss. The
relative magnitude of the two opposing yawing moments is not
known.
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- Ten passengers and a crew of two could be
accommodated in the short, single-step hull formed from a wooden
frame covered with aluminum-alloy sheets. Before passage through
the hump speed, large quantities of spray passed through the
propellers and covered the windshield, effectively blinding the
pilots. Although the aircraft was built for a number of years and
various fixes were attempted, the spray problem on the S-38 was
never effectively solved. Wings of the aircraft consisted of a
metal structure covered with fabric.
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- According to the data in table IV, the S-38B had a gross weight of 10 480 pounds, a
wing span of 71.7 feet, and a top speed of 125 miles per hour.
Although the Sikorsky S-38 was somewhat smaller than the Martin
PM-1, the performance of the two aircraft was nearly the same. The
values of the zero-lift drag coefficient and the maximum lift-drag
ratio were not those of an aircraft known for outstanding
aerodynamic efficiency, but the ruggedness and operational
flexibility of the S-38 made it well suited for many diverse
roles.
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- [187] About 120
examples of the S-38 were constructed, and its configuration
served as a basis for the single-engine S-39 and the large four
engine S-40 flying boat operated by Pan American Airways. The S-41
was a further refinement of the twin-engine S-38, but the
high-drag configuration of this series of aircraft was abandoned
in favor of arrangements of higher aerodynamic efficiency in
subsequent Sikorsky flying boats and amphibians.
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