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Wir sind nicht nur eine Chatseite: A public domain version for a Windows PC can most easily be obtained from cygwin , or also from: Related Software Some pointers to public domain versions of related software packages. It was first publically released in Januaryinitially through the Netlib source code repository. Wir geben deine Adresse nicht weiter, verschicken keinen Spam und sie erscheint auch nirgends in deinem Profil gegen deinen Willen. Zu den weiteren Funktionen der Website gehört die Erstellung eines Benutzerprofils mit der Spin normale version, persönliche Angaben über sich zu machen Kontaktdaten, Interessen, Hobbys etc. Place it, for instance, directly after the opening comments in the file.

Even the display lid is quite warp-resistant. Strong pressure on the back of the display can cause some waves on the display, but these are minimal, which proves how stable the display lid is.

The hinges also offer sufficient resistance. However, shaking the Nitro 5 Spin slightly at an opening angle above 90 degrees does cause the display to open even wider.

However, the overall metal construction appears stable enough and the display does not continue wobbling for very long. The hinges should be tight enough to keep the display in position while using the stylus for inputs.

By the way, the Nitro can be opened with a single hand, as the base is heavy enough to not lift off the table.

However, Acer forgot to add, or decided against, an indentation on the case, which makes opening the device a little more difficult.

Independent journalism is made possible by advertising. We show the least amount of ads whenever possible but we intentionally show more ads when an adblocker is used.

Please, switch off ad blockers and support us! The Acer Nitro 5 Spin has a footprint of As the case has been taken over from the Acer Spin 5 without any changes, the two devices have the same size.

This would be an acceptable weight for a inch notebook, particularly considering the very good workmanship and high-quality material.

But we feel that the Nitro is a little too heavy and large to be used as a tablet. The port selection can be described as mid-range and sufficient.

On the left side, there are two USB 3. The right side offers two status LEDs, the typical volume rocker, a combined 3. If you are a passionate gamer, you might be wondering where the Ethernet port has disappeared to.

Acer has decided that the Nitro, the red gaming version of its Spin 5, does not need a network connector. For real gamers who play online games and are looking for low ping and latency times as well as faultless transmission, this might make the Nitro completely unsuitable.

The power button is not positioned very well for a convertible - if you want to use the Acer as a tablet in portrait mode, you might easily turn the Nitro off by mistake.

Apart from this, the port distribution is very practical, particularly on the left side. The two USB 3. The SD card reader does not have a spring and you simply have to push the SD card into the slot, which is usually the more user-friendly version.

The disadvantage of this method is that the card does not disappear into the slot entirely but always stands out slightly.

In the case of the Nitro 5 Spin, about half of the SD card stands out. The fact that Acer does not offer a network connection via an Ethernet cable for the Nitro is a real shame.

The data transfer rate measured in our benchmark is good and positions the Nitro significantly above the average multimedia device and even puts it slightly over its own non-gaming version Acer Spin 5.

The transfer rate was stable throughout our test and reception was normal. Apart from the fingerprint sensor on the touchpad, the Acer also supports TPM 2.

The Nitro comes with a limited trial period of Norton Security. The Acer Nitro 5 Spin includes a watt power supply, but no other accessories.

An input pen that can be used for the touchscreen, such as the Acer Stylus Pen, has to be purchased separately. The maintenance of the Nitro is not difficult: There are eleven normal Phillips screws that have to be removed in order to lift off the bottom of the base unit.

Closing the device is also easy and fast. The Acer FineTip keyboard and the snugly fitted number block have red lettering that is sufficiently easy to read.

The enter and backspace keys are large enough, but the up and down arrow keys are very narrow and are positioned too close to each other.

The entire keyboard is slightly sunk into the base unit, so that the device can be used easily in tablet mode without the user pressing a key by mistake.

Subjectively, the keys have a cheap, plasticky feeling and they rattle when you run your fingers over them.

The sound when the keys are pressed reminds us not of high-quality material, but rather of thin, lightweight plastic. Nonetheless, the keyboard allows for fast typing and users who type regularly will not have any difficulties.

The rattling keys are not so loud that they become bothersome, but not quiet enough to go unnoticed.

Unfortunately, the keyboard backlighting is a little annoying, as it automatically turns off 30 seconds after the last key was pressed. At night, this means that you regularly find yourself in front of a dark keyboard - even when running on power supply.

There are many entries in various Internet forums from users who are having difficulties with this issue, but it seems like the backlighting cannot be set to run all the time, nor can the duration of the backlighting be adjusted.

It responds well and quickly to inputs with one or two fingers. The ClickPad, however, takes a bit of getting used to as it is hard to make a click above the middle on the left side.

The left bottom area of the touchpad is rather loose and it has two pressure points, similar to the shutter button on a camera. Simply placing the finger on the touchpad is enough to provoke the first click, although this does not do anything and is simply irritating.

Stronger pressure then allows you to make a second, proper click to which the touchpad responds properly. Acer has placed a fingerprint sensor that works quickly and reliably in the top left corner of the touchpad.

A quick placing of the finger on the reader and you are logged-in. The touchpad is large enough for the fingerprint sensor not to get in the way. Acer did not automatically activate the fingerprint reader, as has happened on some other laptops.

The Acer Nitro 5 Spin is equipped with a reflective The display size and resolution result in a pixel density of PPI.

There are no alternative display options for the Nitro. However, they are still too slow for real gamers and you will not get around connecting an external monitor for proper gaming results; IPS displays are not known for their speed, after all.

Only the black value and contrast and the deviations measured with ColorChecker are not as good as those of the Spin 5. So, if a good black value is more important to you than response times or brightness, you might want to take a closer look at the "normal" version of the Spin 5 instead.

I agree that null assignment or lack of assignment should have produced a warning. For any public static variable in a library, probably a warning message should be given even if it was assigned, lets say to string.

This feature the way it was implemented seems problematic to me, since there will be corner cases when compiler does not ensure null safety since it does not claim to do so.

I am super-excited to use the new language features! I already started porting part of our product to be released late so as to play with, amongst other things, the nullable reference types.

I do have a couple of questions not sure if this is the right place to ask these: The concept of non-null strings might be better if you can enforce non-nullability for all cases, including array initialization, unsafe and interop statements, legacy method calls, etc.

User will have to suppress all such warning explicitly but they will at least be aware of possible pitfalls.

I absolutely love it! I also dislike the idea of default implementations for interfaces, but I can see how it can make life easier…. The new features are awesome!

Second range index being exclusive is downright scary and is going to cause a lot of cognitive dissonance. The world now has to remember that first index is actually index, and second index is a 1-based number — what kind of convenience is that?

You are iterating from index 1 to index 3! How hard is it to just treat the second index as index, and not as a number? If you wanted to be consistent with C, you would treat both components as indexes.

This comment right here is aces. More beautiful syntax for it and ends the religious debate and allow everyone continue to make off by 1 errors.

Those should be supported, but I do not like your syntax. The new features are great. When this one is coming? If you have the project settings set to have warnings as errors, the nullable warnings are errors.

What if we use a library and the library uses by default the old string null ability? VS preview error — I enabled c 8 on a.

After I build the app the Error list windows shows many warnings but any time I click on one of them to go to the code location the warning disappears from the Error list window!

Is c 8 not available for. Nullables — great, but I only hope the settings will allow to use the new syntax but without actual checking anything.

Such case would be useful for transition without it, it will be much harder. Ranges, nice, but I am waiting for spread operator for yields.

Good choice with Nullable reference types it proved itself very nicely in Kotlin. Have you ever thought about introducing val keyword for implicit declarations of read-only local variables?

What about a step-syntax? Is there a legitimate reason for the terminal index on ranges being exclusive? It is simply unintuitive and I cannot fathom a reason for it.

It seems wrong to assume that something should default to being non-null when it could be null. In my mind that seems the safer and more correct decision to assume the opposite of what you have.

Will the templates for all new C projects be modified to ensure they produce nullable safe starting points with no warnings, and provide examples of good practice?

Why not chosen for:. Why not use reference required types instead of non- nullable reference types? For example, following means the variable is not nullable.

And following still work as before. So that there will not be a lot of problems, like default and compatibility. Although it introduces a new concept.

The example given for Nullable Reference Types could blow up with string. Empty input with an IndexOutfRangeException , maybe something like:.

How can I add block of code in the comment section? Several of the deleted comments are my attempts…. Is there any talk into bringing back private field creation and instantiation in the constructor like typescript.

I feel like I am constantly typing the same thing over and over with all the IOC being used nowadays. I feel like it was talked about and retracted, but a refresher on the reasoning would be nice.

I do acknowledge the expression body way of doing this utilizing tuples. I think Microsoft is moving in the wrong direction.

As more of those technologies are introduced by the Open Source community VS 20xx will become more and more redundant.

Microsoft is not investing resources in it and I am afraight they will lose a lot of young developers because they will go with the flow, and that flow is not Microsoft.

Umbraco is a mess. Orchard has I believe one Microsoft developer. The big question is: Should you use still use VS?

Is there something else that we must install or add?? This is all fine , except the files that trigger the warnings are designer-generated.

It seems the EF and WPF designers must still be updated to produce code that cooperates with nullable references?

I followed the instructions at the top of the post but was getting no warnings. My project file looks like.

Sorry about the formatting, This blog seems to reformat and remove text when I post stuff. I assume there is some sort of markdown stuff going on but there is no documentation or help.

Can you explain this in more detail? Getting ready First of all, download and install Preview 1 of. Nullable reference types The nullable reference types feature intends to warn you about null-unsafe behavior in the code.

The first one is on the null in this line: The trailing question mark signals that null is allowed: Until the next line of code! There are a couple of ways in which a null may slip through and cause a null reference exception: The analysis itself has certain holes.

Most of them are a trade-off between safety and convenience; if we complained, it would be really hard to fix.

For instance, when you write new string[10] , we create an array full of nulls, typed as non-null string s. For instance, the line we started out with: Ranges and indices C is getting more expressiveness around working with indexed data structures.

Go ahead and change your program to the following: Generic; using static System. Modify the foreach as follows: If we wanted, we could pull it out into its own variable, and it would work the same: Delay ; yield return name; Of course we get an error that you can only await in an async method.

Next steps Please let us know what you think! NET Core c visual studio. Join the conversation Add Comment. Cancel You must be logged in to post a comment.

Is the following line valid with Nullable Reference Types, and if so what is the result? Is it possible use c 8 on Linux?

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A pilot who is overshooting the turn to final approach may be tempted to apply more rudder to increase the rate of turn.

The result is twofold: Reacting to these unintended changes, the pilot then begins to pull the elevator control aft thus increasing the angle of attack and load factor while applying opposite aileron to decrease bank angle.

Taken to its extreme, this can result in an uncoordinated turn with sufficient angle of attack to cause the aircraft to stall. This is called a cross-control stall , and is very dangerous if it happens at low altitude where the pilot has little time to recover.

To avoid this scenario, pilots learn the importance of always making coordinated turns. They may simply choose to make the final turn earlier and shallower to prevent an overshoot of the runway center line and provide a larger margin of safety.

Certificated, light, single-engine airplanes must meet specific criteria regarding stall and spin behavior.

Spins are often entered intentionally for training, flight testing, or aerobatics. In aircraft that are capable of recovering from a spin, the spin has four phases.

At low altitude spin recovery may also be impossible before impacting terrain, making low and slow aircraft especially vulnerable to spin related accidents.

These four modes are defined by the angle of attack of the airflow on the wing. During the s NASA used its spin tunnel at the Langley Research Center to investigate the spinning characteristics of single-engine general aviation airplane designs.

Some tail designs that caused inappropriate spin characteristics had two stable spin modes — one steep or moderately steep; and another that was either moderately flat or flat.

Recovery from the flatter of the two modes was usually less reliable or impossible. The further aft that the center of gravity was located the flatter the spin and the less reliable the recovery.

Single-engine airplane types certified in the normal category must be demonstrated to recover from a spin of at least one turn, while single-engine aircraft certified in the utility category must demonstrate a six turn spin that cannot be unrecoverable at any time during the spin due to pilot action or aerodynamic characteristic.

In early aviation, individual pilots explored spins by performing ad-hoc experiments often accidentally , and aerodynamicists examined the phenomenon.

Parke attempted to recover from the spin by increasing engine speed, pulling back on the stick, and turning into the spin, with no effect.

The aircraft descended feet, and horrified observers expected a fatal crash. Though disabled by centrifugal forces, Parke still sought an escape.

In an effort to neutralize the forces pinning him against the right side of the cockpit, he applied full right rudder, and the aircraft leveled out fifty feet [16] above the ground.

With the aircraft now under control, Parke climbed, made another approach, and landed safely. The first documented case of an intentional spin and recovery is that of Harry Hawker.

In , the English physicist Frederick Lindemann conducted a series of experiments in a B. In Britain, starting in , spin recovery procedures were routinely taught by flight instructors at the Gosport School of Special Flying, while in France, at the School of Acrobacy and Combat, Americans who had volunteered to serve in the famous Lafayette Escadrille were by July learning how to do what the French called a vrille.

During the s and s, before night-flying instruments were commonly available on small aircraft, pilots were often instructed to enter a spin deliberately to avoid the much more dangerous graveyard spiral when they suddenly found themselves enveloped in clouds, hence losing visual reference to the ground.

In almost every circumstance, the cloud deck ends above ground level, giving the pilot a reasonable chance to recover from the spin before crashing.

Today, spin training is not required for private pilot certification; added to this, most training type aircraft are placarded "intentional spins prohibited".

Generally, though, spin training is undertaken in an "Unusual attitude recovery course" or as a part of an aerobatics endorsement though not all countries actually require training for aerobatics.

However, understanding and being able to recover from spins is certainly a skill that a fixed-wing pilot could learn for safety. It is routinely given as part of the training in sailplanes , since gliders often operate slowly enough to be in near-stall conditions while turning.

Because of this, in the U. Also, before their initial certifications both airplane and glider instructors need a logbook endorsement of proficiency in spin training which, under Federal Aviation Regulations Some aircraft cannot be recovered from a spin using only their own flight control surfaces and must not be allowed to enter a spin under any circumstances.

If an aircraft has not been certified for spin recovery, it should be assumed that spins are not recoverable and are unsafe in that aircraft.

Spin-entry procedures vary with the type and model of aircraft being flown but there are general procedures applicable to most aircraft. These include reducing power to idle and simultaneously raising the nose to induce an upright stall.

Then, as the aircraft approaches stall, apply full rudder in the desired spin direction while holding full back-elevator pressure for an upright spin.

Sometimes a roll input is applied in the direction opposite of the rudder i. If the aircraft manufacturer provides a specific procedure for spin recovery, that procedure must be used.

Otherwise, to recover from an upright spin, the following generic procedure may be used: Power is first reduced to idle and the ailerons are neutralized.

Then, full opposite rudder that is, against the yaw is added and held to counteract the spin rotation, and the elevator control is moved briskly forward to reduce the angle of attack below the critical angle.

Depending on the airplane and type of spin, the elevator action could be a minimal input before rotation ceases, or in other cases the pilot may have to move the elevator control to its full forward position to effect recovery from the upright spin.

Once the rotation has stopped, the rudder must be neutralized and the airplane returned to level flight. Inverted spinning and erect or upright spinning are dynamically very similar and require essentially the same recovery process but use opposite elevator control.

In an upright spin, both roll and yaw are in the same direction, but an inverted spin is composed of opposing roll and yaw.

It is crucial that the yaw be countered to effect recovery. The visual field in a typical spin as opposed to a flat spin is heavily dominated by the perception of roll over yaw, which can lead to an incorrect and dangerous conclusion that a given inverted spin is actually an erect spin in the reverse yaw direction leading to a recovery attempt in which pro-spin rudder is mistakenly applied and then further exacerbated by holding the incorrect elevator input.

In some aircraft that spin readily upright and inverted, such as Pitts- and Christen Eagle-type high-performance aerobatic aircraft, an alternative spin-recovery technique may effect recovery as well, namely: Before spinning any aircraft, a pilot should consult the flight manual to establish if the particular aircraft type has any specific spin recovery techniques that differ from standard practice.

A pilot can induce a flat spin once the spin is established by applying full opposite aileron to the direction of rotation—hence, the requirement to neutralize ailerons in the normal spin recovery technique.

The aileron application creates a differential induced drag that raises the nose toward a level pitch attitude. As the nose comes up the tail moves out farther from the center of rotation increasing lateral airflow over the empennage.

Recovery is initiated by maintaining pro-spin elevator and rudder and applying full aileron into the spin.

Differential drag now lowers the nose returning the plane to a normal spin from which the PARE technique is used to exit the maneuver.

Although entry techniques are similar, modern military fighter aircraft often tend to require yet another variation on spin recovery techniques.

While power is still typically reduced to idle thrust and pitch control neutralized, opposite rudder is almost never used.

Adverse yaw created by the rolling surfaces ailerons, differential horizontal tails, etc. Hence, the preferred recover technique has a pilot applying full roll control in the direction of the rotation i.

Likewise, this control application is reversed for inverted spins. The characteristics of an airplane with respect to spinning are significantly influenced by the position of the center of gravity.

In general terms, the further forward the center of gravity the less readily the airplane will spin, and the more readily it can recover from a spin.

Conversely, the further aft the center of gravity the more readily the airplane will spin, and the less readily it can recover from a spin.

In any airplane, the forward and aft limits on center of gravity are carefully defined. In some airplanes that are approved for intentional spinning, the aft limit at which spins may be attempted is not as far aft as the aft limit for general flying.

For this reason, pilots should first determine what "tendency" the airplane has before it stalls. If the tendency is to pitch down nose-heavy when it stalls, then the aircraft is likely to recover on its own.

However, if the tendency is to pitch up tail-heavy when it stalls, the aircraft will likely transition into a "flat-spin" where stall recovery would be delayed, or it may not be recoverable at all.

If it pitches down, then the aircraft is stall recoverable. If the nose pitches up, then the stall would be difficult to recover or altogether unrecoverable.

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