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Thank you, MJolner for your comments.
I read your comment about there being no “mention of AOA or pitch angle”. I take it that your concern is with the pilot’s ability to see the runway ahead when on approach.
As you know, there is no AOA indicator in the P-47. It was not until fairly modern times that military jets began to have a numerical AOA readout on their HUDS, and/or a simple three symbol AOA indicator to aid the pilot in controlling the landing approach. Accordingly, the ‘47 pilot has no way of precisely knowing what the actual AOA is at any given time.
In any event, I don’t think that AOA (the angle of the mean chord to the relative wind) is the main issue with regard to your concern about vision over the nose. As you know, the performance of an airplane at any given moment is determined by many factors: density altitude, airspeed, power, and rate of altitude change. In my cadet days, a hundred years or so ago, I was taught that: Performance = power + attitude.
Pitch angle (the angle of the aircraft’s mean chord line to the horizon) seems to be what you are talking about. The aircraft’s pitch angle can be measured to an approximate degree of accuracy with the simple gyro horizon the P-47. More modern, ball-type attitude indicators and glass cockpits have exact pitch-degree readouts; but, of course, these were not yet invented in the ’47’s day. The basic gyro horizon in the ’47 can be interpreted with reference to needle widths: 1 needle width = approximately 5 degrees of pitch. I went back (I was about to say “up”, it seems so real to me to fly the A2A ’47), and flew an approach routine, but this time with one eye on the gyro horizon and the other on the real horizon.
While pilot’s performance reports of aircraft from the era of the ’47 do not traditionally include the pitch angle as part of the data; because this is sim flying, we can make our own rules. I measured the gyro horizon readout by needle widths. The pitch angle relative to the actual horizon is my best visual estimate. This is what I found:
Standard day, 0 wind, 0 turbulence, below 2000’, 738 lbs. (123 U.S. Gal.) of fuel on board, no ammunition, gear down, canopy open –
@30 in. Hg, 2,550 rpm Level Flight - Flaps up, 130 mph Pitch Angle - Gyro Horizon: +1 needle, Actual Horizon: +5 degrees
25 degrees flap, 120 mph Pitch Angle - Gyro Horizon: +2 needles, Actual Horizon: +10 degress
Final approach descent- 25 degrees flap, 125 mph,-500 fpm Pitch Angle -Gyro Horizon:+½ needle. Actual Horizon: +2 degrees 40 degrees flap, 125 mph,-1,200 fpm Pitch Angle -Gyro Horizon: -1/2 needle, Actual Horizon: -2 degrees
@35 in. Hg, 2,550 rpm Level Flight- Flaps up, 145 mph Pitch Angle - Gyro Horizon: +1 needle, Actual Horizon: + 5 degrees
25 degrees flap, 120 mph Pitch Angle-Gyro Horizon:+1-1/2 needles, Actual Horizon +7 degrees
Final Approach descent - 25 degrees flap, 125 mph, -250 fpm Pitch Angle - Gyro Horizon: +1 needle, Actual Horizon: +5 degrees
40 degrees flap, 125 mph, -1000 fpm Pitch Angle - Gyro Horizon: level, Actual Horizon: level
I agree that the ’47 is very “agreeable” regarding visibility on landing approach. However, not all R-2800 powered aircraft had good over-the-nose visibility on approach. The F4U was notoriously poor in this department. The type of engine used is not a factor regarding forward visibility, except that an inline engine is narrower, of course, and you can usually see around it a bit better than a massive radial. Still, most of the taildragger fighters of that era, whether in-line or radial engined, had poor forward vision on the landing approach. That is why so many inventive landing approach methods, some of which I mentioned, were used by pilots of all types of fighters.
I don’t know what it may be that some pilots are doing that is causing them grief. They may not be following the prescribed procedures, and using the correct power, flaps and airspeeds. To anyone out there who is having trouble landing the ’47, I’d appreciate it it if you would let me know what the problem is. Be sure to note and tell me the altitude of the field, the weather conditions (wind, temperature and pressure), your fuel and any ordinance on board, what the power settings, airspeeds, altitudes, and flap settings are that you are using on approach, and anything else that will help me to understand your situation.
I prefer using 35 in. Hg, and 2550 rpm in the pattern and approach. I fly base at 1000’ AGL turning final and dropping flaps to 25 degrees; then, descending at 125 mph, with flaps at 25 degrees, -250 fpm, I have a very good view of the runway. At mid-final, descending with flaps at 40 degrees, - 1,000 fpm and maintaining 125 mph, a good portion of the runway remains in view all the way down. I flair high and I like wheel landings, either level or slightly tail low, as I can see the runway until the tail finally comes down.
You’re absolutely right about the unorthodox landing methods which many fighter pilots adopted. Lots of things that pilots in the combat theatres did with their aircraft were not contemplated by the engineers and test plots who went by, and in many cases wrote the book on these aircraft. The exuberance of youth is often at odds with, and tests the limits (and patience) of orthodoxy. If we’re lucky, someday we can look way back and laugh at what we did when we were indestructible and immortal.
While it's true that many of the aircraft used in WWII were purposely designed so that relatively inexperienced pilots of average skill could fly them successfully, there were still many training accidents, often fatal; and there were many tragic losses due to pilot error, even after assignment.
As flying the A2A P-47 informs us, some of the fighters of that era were fairly complex to operate, and challenging to fly properly. The American aviation cadets of the WWII era, some of whom had never even been a passenger in an airplane before entering the service, had hundreds of hours of stick time in various aircraft of increasing complexity, performance, weight and size before they were permitted to fly combat aircraft. The washout rate for pilot cadets was very high (I don’t know the exact figures, if someone does, please let me know), a practice which saved many lives.
In the era of the P-47, if you were a cadet fresh out of training who was assigned to fly a single-seat fighter, your first flight in it was solo. You may have seen a training film, gotten a cockpit check on the ground, and few tips from an experienced hand; but that was all. You read the Dash -1, got in the bird, fired it up, and flew it.
The Hellcat, SBD and Avenger were, reportedly fairly docile; but the ’47 took its fair toll of cadets, as did the F4U, which was particularly unforgiving and vicious at slow speeds, even for skilled and experienced pilots. They were all predictable; it’s just that in some aircraft, what was predicted was not always pleasant.
These extremely fast, heavy and powerful (for those days) single- seat airplanes of WWII were something new, and they were the equivalent to the pilots of those days to the latest stealth, Mach 2+ jet fighters of today. We have the benefit of decades of experience with high performance aircraft, and how to train pilots to fly them that no one yet had in the ’40s. The first military, all-metal monoplanes with retractable gear and closed canopies did not come into being until the middle of the 30’s. It was only a few years later that the advent of the 2,000+ hp airplane which flew at 35,000’ and over 400 mph, began.
Your approach method seems sound; and if it’s working for you, great.
Amen to your observation about people who compare Cessna 172s and Playstation airplanes to the A2A P-47 and A2A’s other aircraft. We’ll just have to patiently help them along, and help them learn how to fly high-performance airplanes that fly realistically. Once they've experienced the joy and satisfaction of it, they’ll never go back. Mitchell
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