A method for calculating the pressure distribution over jet-flapped wings / by D. Küchemann.
The incompressible flow past an aerofoil with a thin jet emerging from its lower surface somewhere near the trailing edge is considered. A simple method is described for calculating the pressure distribution over wings of non-zero thickness. The possible effects of sweep are briefly discussed. It...
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| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Format: | Book |
| Language: | English |
| Published: |
London :
H.M.S.O,
1957.
|
| Series: | Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
no. 3036. |
| Subjects: |
MARC
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| 100 | 1 | |a Küchemann, Dietrich, |d 1911-1976. |0 http://id.loc.gov/authorities/names/no2007041583 |1 http://isni.org/isni/0000000083825745. | |
| 245 | 1 | 2 | |a A method for calculating the pressure distribution over jet-flapped wings / |c by D. Küchemann. |
| 260 | |a London : |b H.M.S.O, |c 1957. | ||
| 300 | |a 25 pages : |b illustrations ; |c 31 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a Reports and memoranda ; |v no. 3036. | |
| 504 | |a Includes bibliographical references (page 17) | ||
| 500 | |a "May 1956" | ||
| 500 | |a "R.A.E. report Aero. 2573, received 2nd June, 1956." | ||
| 520 | |a The incompressible flow past an aerofoil with a thin jet emerging from its lower surface somewhere near the trailing edge is considered. A simple method is described for calculating the pressure distribution over wings of non-zero thickness. The possible effects of sweep are briefly discussed. It is pointed out that a saddleback chordwise loading is typical for aerofoils with jets and that this is the basic reason for many of the aerodynamic advantages of the jet-flap system. | ||
| 650 | 0 | |a Aerodynamic load |x Mathematical models. | |
| 650 | 0 | |a Aerofoils |x Aerodynamics. | |
| 650 | 7 | |a Incompressible flow. |2 nasat. | |
| 650 | 0 | |a Jet flaps (Airplanes) |x Aerodynamics |x Mathematical models. | |
| 710 | 2 | |a Aeronautical Research Council (Great Britain) |0 http://id.loc.gov/authorities/names/n80076393 |1 http://isni.org/isni/0000000121783487. | |
| 710 | 2 | |a Royal Aircraft Establishment (Great Britain) |0 http://id.loc.gov/authorities/names/n80126349. | |
| 830 | 0 | |a Reports and memoranda (Aeronautical Research Council (Great Britain)) ; |v no. 3036. |0 http://id.loc.gov/authorities/names/n84728012. | |
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