「Airspeed」の共起表現一覧(1語右で並び替え)
該当件数 : 96件
The | Airspeed A.S.39 Fleet Shadower was a British long-rang |
which provide additional information such as | airspeed, altitude and outside air temperature. |
formation from the sensors, such as air data ( | airspeed, altitude). |
An instrument panel showing the | airspeed, altitude, and other details required for nav |
Position error affects the indicated | airspeed and the indicated altitude. |
culated as one of the steps between indicated | airspeed and true airspeed; |
is shown as the difference between indicated | airspeed and equivalent airspeed. |
provided by the system, giving things such as | airspeed and battery voltage. |
Airspeed and altitude data were lost, the aircraft dep | |
ght of the attitude indicator are usually the | airspeed and altitude indicators, respectively. |
-around the plane stalled due to insufficient | airspeed and crashed in the sea at 16:40 Hrs. |
to publish details of the error in indicated | airspeed and indicated altitude across the operating r |
sna 182s and Cessna 210s, did not provide the | airspeed and safety needed for the department's new ai |
marker above the glide slope at an excessive | airspeed and thereafter compounded by the flightcrew's |
These factors include | airspeed, angle of attack, aircraft weight, accelerati |
On 6 February 1958, an | Airspeed AS 57 Ambassador charter plane crashed soon a |
The | Airspeed AS.45 Cambridge was a British advanced traine |
nd climb at approximately the same calibrated | airspeed at any elevation, even though the true airspe |
light information, such as heading, attitude, | airspeed, barometric and radio altitude, vertical spee |
aircraft, and making appropriate altitude and | airspeed callouts is always clearly assigned to one cr |
es”, which scroll up and down as altitude and | airspeed change. |
ent failure and loss of critical attitude and | airspeed data. |
During this time the jet's | airspeed decreased from 270 to 215 knots and as the pe |
to stabilize the aircraft's descent rate and | airspeed, descended below the glideslope and drifted a |
mic stability problems, but not as bad as the | Airspeed design which was cancelled in February 1941. |
are able to read groundspeed (and often true | airspeed) directly, without calculating calibrated air |
n-standard actions resulted in severe loss of | airspeed due to the propeller blades being accidentall |
descent, the FDR recorded an increase in the | airspeed from 300 to 800 km/h in three seconds, which |
t aircraft to dive into the sea as sufficient | airspeed had not been gained. |
Airspeed Horsa | |
rachute Brigade in Normandy as well as towing | Airspeed Horsa gliders across the English Channel. |
e T-2 hangars were added specifically for the | Airspeed Horsa gliders which were to be stored at this |
Research's strip heating process to assemble | Airspeed Horsa gliders, as did de Havilland on its Mos |
function, along with restoring or building an | Airspeed Horsa, an American CG-4A Waco and a De Havill |
werful tugs were not available for the larger | Airspeed Horsa. |
For airspeeds (TAS) over Mach 0.2, as | Airspeed increases the temperature exceeds that of sti |
Illustration of the | airspeed indication and detection system on fly-by-wir |
Installation of true | airspeed indicator |
Airspeed indicator diagram showing pressure sources fr | |
Since the | airspeed indicator capsule responds to impact pressure |
t, it is the speed which would be shown by an | airspeed indicator with zero error. |
same color scheme is used as on a mechanical | airspeed indicator to represent the V speeds. |
Airspeed indicator markings use a set of standardized | |
The | airspeed indicator displays the speed of the aircraft |
in any mechanical parts (unlike an aircraft's | airspeed indicator and altimeter). |
In addition, there was no | airspeed indicator, the ball turret was jammed with th |
itot/static and vacuum operated instruments:- | Airspeed indicator, altimeter, climb/descent indicator |
The Pitot tube supplies pressure to the | airspeed indicator. |
that a pilot can read them directly from the | airspeed indicator. |
e single instrument is the "maximum allowable | airspeed indicator." |
d operation of ships, low speed aircraft, and | airspeed indicators for low speed aircraft - that is a |
g glass cockpit instrument systems employ two | airspeed indicators: an electronic indicator on the pr |
heet foam, Hefty Express shipping mailers and | AirSpeed inflatable packaging systems and materials. |
Airspeed information is also sent to the autoflight su | |
Airspeed information is also sent to the flight comput | |
any aircraft, the effect of position error on | airspeed is shown as the difference between indicated |
The wings support the aircraft when | airspeed is high enough. |
At high speeds and altitudes, calibrated | airspeed is further corrected for compressibility erro |
ircraft such as the Space Shuttle, equivalent | airspeed is calculated instead of calibrated airspeed. |
The | airspeed is typically presented in the form of a "tape |
ham was also one of the founding directors of | Airspeed Limited, the aircraft manufacturing company s |
Norway and Tiltman formed | Airspeed Ltd in 1931, where he designed several basic |
British aircraft designer, and co-founder of | Airspeed Ltd. |
Shute Norway) who was one of the founders of | Airspeed Ltd. |
ual instruments, can determine the calibrated | airspeed, Mach number, altitude, and altitude trend fr |
, a VDI and a HSD display, that gives data on | airspeed, navigation and other information. |
is the True | Airspeed of the aircraft, TAS. |
It is widely used to determine the | airspeed of an aircraft and to measure air and gas vel |
It is believed that the craft reached an | airspeed of 335 knots, fully 15 percent more than the |
ot Lieutenant Funabashi reach a maximum level | airspeed of 624 km/h (387 mph) in the second prototype |
reference, specifically to the gag about the | airspeed of unladen swallows in Monty Python and the H |
For an aircraft engine, changes in | airspeed or altitude cause changes in air speed and de |
ncluded wings for De Havilland Tiger Moth and | Airspeed Oxford trainers, wing flaps for Fairey Barrac |
Advanced Training Flying Unit, equipped with | Airspeed Oxford trainers. |
Force moved in, along with Hawker Hurricane, | Airspeed Oxford and Avro Anson aircraft. |
l squadrons, with the main aircraft being the | Airspeed Oxford. |
o. 9 Group RAF who flew Hawker Hurricanes and | Airspeed Oxfords from the site. |
He then trained on twin-engined | Airspeed Oxfords at Little Rissington before moving to |
monoplane training began on the first of 229 | Airspeed Oxfords in 1938. |
No. 21 Group Flying Training Command, flying | Airspeed Oxfords and conducting navigation and cross-c |
oard Miles Masters, Boulton Paul Defiants and | Airspeed Oxfords in 1942, Miles Martinets and Spitfire |
Beaufighter, while the squadron also had some | Airspeed Oxfords on strength for training and communic |
The RAF decided to recapture the flight | airspeed record with its new generation of jet aircraf |
orthodox aircraft intended to break the world | airspeed record for a piston-engined aircraft. |
During World War II, most of the pre-war | airspeed records had been broken. |
nflicts, Bruno was involved in setting flight | airspeed records in a 1938 flight to Brazil. |
Furthermore the IAS is specified in regard to | airspeed restrictions below certain altitudes since it |
and handling suffered greatly under 90 knots | airspeed, since the speed of approach to land on a car |
He left | Airspeed soon after, and in 1948 co-founded Tiltman La |
At low heights with low | airspeed, such as a hover taxi, the pilot can simply c |
t instrument that shows the ratio of the true | airspeed to the speed of sound, a dimensionless quanti |
tion seats, rated from zero altitude and zero | airspeed up to 450 knots. |
a, it still uses the system to make altitude, | airspeed, vertical speed, and other measurements preci |
ed too far along the runway and its touchdown | airspeed was excessive, both of which could contribute |
General Aircraft and | Airspeed were selected to build two prototypes each an |
in height without a corresponding increase in | airspeed will put the aircraft above a survivable un-c |
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