| UNIVERSITY OF GENOA FACULTY OF ENGINEERING HYDRAULIC INSTITUTE

## GALLERY

I am planning to include in this page all the photo and images people sent me together with some description.

I would like to extend this section, so please email me any image you feel is pertinent to this project. Be sure to include a few lines of description of what can be seen in the image.

- Thanks to Jan-Olov Newborg who sent me picture 1, 2, 3, 6 and 7. Well ... this makes 5 over a total of 7! Thanks a lot Jan.
- I have uploaded pictures 4 and 5 and the description of picture 1 from here
- Thanks to Bill Beaty for the description of picture 3.

## (1) |  | Trailing vortices and downwash phenomenon of an aircraft in flight are seen clearly in this figure. In this situation, a Cessna Citation VI was flown immediately above the fog bank over Lake Tahoe at approximately 313 km/h or 170 knots (B. Budzowski, Director of Flight Operations, Cessna Aircraft Company, private communication, 1993). Aircraft altitude was about 122 m (400 ft) above the lake, and the weight was approximately 8400 kg. As the trailing vortices descended over the fog layer due to the downwash, the flow field in the wake was made visible by the distortion of the fog layer. The photo was taken by P. Bowen for the Cessna Aircraft Company from the tail gun- ner's position in a B-25 flying in formation slightly above and ahead of the Cessna. The aircraft is seen initiating a gentle climb after a level flight, leaving a portion of the fog layer yet unaffected. The wing span measured 16.3 m and the wing area was 29 m^2. The Reynolds number based on the mean aerodynamic chord of 2.1 m was 1.1x10^7. Extract from the Gallery of Fluid Motion, Physics of Fluids A, Vol. 5, September 1993. Contribution by Hiroshi Higuchi (Syracuse University). Photo courtesy of Cessna Aircraft Company.

I think this picture is of the same set of picture (1). The Author is again Paul Bowen. |  | ## (2)

## (3) |  | Fluid simulation from SAAB Aircraft shows phase lag between upper and lower air parcels after an airfoil has passed. Air travels much faster over the top of the airfoil, and then it never rejoins the air which has travelled below. Note that the airfoil has deflected the air downwards.

On a clear day, trailing vortices are often seen in the sky following the passage of an airplane. The vortices are formed because the wing develops lift. That is, the pressure on the top of the wing is lower than on the bottom, and near the tips of the wing this pressure difference causes the air to move around the edge from the bottom surface to the top. This results in a roll-up of the fluid, which then forms the trailing vortex. In the sky, the vortex becomes visible when the air has a high humidity. The velocities inside the vortex can be very high, and the pressure is therefore quite low. Water vapor in the air condenses as water droplets, and the droplets mark the presence of the vortex. In this picture of a cropduster flying near the ground, the vortex is made visible by a red flare placed on the ground. The red smoke is wrapped up by the trailing vortex originating near the tip of the wing. The strength of the vortex is related to the amount of lift generated by the wing, so they become particularly strong in high-lift conditions such as take-off and landing. They also increase in strength with the size of the airplane, since the lift is equal to the weight of the airplane. For a large transport airplane such as a 747, the vortices are strong enough to flip a small airplane if it gets too close. Trailing vortices are therefore the principal reason for the time delay enforced by the FAA between take-offs and landings at airports. Picture courtesy of DANTEC Measurement Technology. |  | ## (4)

## (5) |  | Another picture from the 1993 Aviation Week & Space Technology Photo Contest. This came second in the Military catergory, and it was taken by James E. Hobbs, from Lockheed Aircraft service Co., Ontario, California. The plane is ejecting flares during a test of an infrared missile warning and self-protection system installed on a C-130 Hercules. The trailing vortices formed in the wake are clearly visible. The size of these vortices is related to the lift produced by the wings, and the photograph suggests that the aircraft was climbing during this maneuver.

| This picture shows a SAAB JAS39 Gripen landing on a rainy roadbase. Downwash is made evident by the foggy cloud above the runaway. |  | ## (6)

## (7) |  | Some more downwash ... this is a French Transall deploying flares.