...JULY 15TH, 1948 FLIGHT 79
The Gyrodyne
words, the normal operating condition of the gyrodyne is with
both the fuselage and the tip-path plane substantially level.
Periodic Blade-tip Stall
At one time ...
1948 - 1091.pdf
|
...FLIGHT, II May 1951 567
(Above) The 240-lb thrust Turbomeca Pimene.
(Right) Comparison between the two Avro Canada
turbojets—Chinook (2,600 Ib thrust) and the
larger Orenda, rated at over 6,000 Ib.
JE...
1951 - 0906.pdf
|
...RIGHT International, 5 January 1967 23
AERO ENGINES
A "Flight" Survey
THE ADVENT OF SUPERSONIC TRANSPORTS, the big long-rangesubsonic transport, the Vietnam war, and major newequipment programmes for ...
1967 - 0021.pdf
|
...34 HJGHT International, 6 January I9U
Lycoming T53-L-I3 free-turbine turboshaft. Five-
stage axial plus single-stagecentrifugal compressor
with single-sided impeller.Annular reverse-flow com-
bustion ...
1966 - 0044.pdf
|
...FUGHT International, 19 January 1980 175
World Light
Turbine Directory
SO-3 single-shaft turbojet for the
TS-11 Iskra trainer. PZL is now the
sole manufacturer of the GTD-350
and has developed i...
1980 - 0185.pdf
|
...MILITARY PROPULSION
Left RTM.322 has a single-shaft core, plus an output shaft driven by a free turbine. Rolls-Royce and Turbomeca have equal shares in its development
and production. Right RTM.322,...
1984 - 0686.pdf
|
...FLIGHT JANUARY 6TH, 1949
BOOK REVIEWS
Aircraft—from Airships to Jet Propulsion. By B. W. A.
Dickson. First impression, private issue, then Naldrelh
Press. Price &s Gd.
HPHIS is the season when the aer...
1949 - 0036.pdf
|
...58
flow 2421b/sec, length 235 -7in, diameter 50-7in, weight
4,1761b.
TF33 (JT3D) Two-shaft turbofan. This is the military
version of the commercial JT3D turbofan.
Variable-Cycle Engine Two-shaft ...
1978 - 0046.pdf
|
...IfUGHT International. 6 lanuary 1966 35Despite the selection of the General Elec-tric GE1/6 engine for this application,Pratt & Whitney has announced that it is
continuing with development of the
41 o...
1966 - 0045.pdf
|
...*0
70
40 V
VX
s\
SINGLE STAGE >5;
*"
STAG!: co
>^=
MmOS)
««.
|
MULTI-STAGE COMWESSOR '*
1— N Aim UDC TEST F
|
iNT
NOTE-REYNOLDS NUMBER
6ASC0 ON MEAN BLADE
CHORD. AND MEAN BLAC
SPEED.
/N ON-SYMMETRIC
'...
1957 - 1832.pdf
|
...566 FLIGHT, II May 1951
DESIGNS OF A DECADE . . .
small combustion chamber the hot gases are manifolded to the
intake and are exhausted into the inlet stream, the temperature of
which is so raised as ...
1951 - 0903.pdf
|
...12 FLIGHT 29 JUNE 195t
UNITED CO.PO.M"!
Dear Sir:
The requirements of the Korean campaign, the expansion of our military forces
and the needs of both domestic and foreign airlines are such that United...
1951 - 1215.pdf
|
...FUGHT
International,
6 January
1966
SNECMA TFI06 twin-spool turbofan with reheat. Three-stage axial fan plus six-stage axial intermediate compressor, seven-stage axial h-p compressor of 249lb/sec mass...
1966 - 0031.pdf
|
...18 FLIGHT 30 NOVEMBER I9J
UNITED
UN,,ED AIRCRAFT EXPORT
PRATT & WHITNEY J-4.2 AUTHORIZED 1.000 HOURS BETWEEN OVERHAULS —The Pratt & Whitney
J-42 Turbo-Wasp has recently become the first U.S. jet aircr...
1951 - 2359.pdf
|
...13 JUNE 1952 FLIGHT 3
PROCESS FOR NICKEL COATING OF ALUMINUM TO PROLONG PROPELLER BLADE LIFE —Development
of a process for nickel coating of aluminum, hitherto considered impossible, was an
nounced...
1952 - 1627.pdf
|
...Rolls-Royce Spay 25 twin-spool
turbofan with reheat. Five-stage axial
|-p compressor (fan), 12-stage axial
h-p compressor. Cannular straight-
through-flow combustion chamber
with ten flame tubes. Two-...
1966 - 0029.pdf
|
...20 March 1959
AERO ENGINES 1959 . . .
being fitted to the Convair F-106 and RepublicF-105 families. Both engines are equipped with
variable afterburners and are stressed for flightat Mach numbers slig...
1959 - 0820.pdf
|
...FLIGHT 8 FEBRUARY 1952
.... ,..••••
UNITED AIRGRAM
^ "UH.T.D ^J™°r^X^
PRATT & WHITNEY TO POWER BIGGEST U.S. MILITARY TRANSPORTS —Two of the world's
biggest air transports now in production will b...
1952 - 0326.pdf
|
...f
698 FLIGHT
TWO-SPOOL TURBO-WASP . . .
Force would be prepared to pay extra for a really efficient engine.
At the start, the J57 was visualized as a big axial to give
10,000 lb thrust. To meet t...
1953 - 1544.pdf
|
...2 FLIGHT 12 FEBRUARY 1954
UNITED AIRCRAFT EXPORT CORPORATION
1-57 OFFICIALLY RATED IN 10,000-POUND THRUST r CLASS w
The J-57, Pratt & Whitney Aircraft's big, new turbojet engine, has been officiall...
1954 - 0358.pdf
|