Oscillating supersonic delta wings with curved leading edges
In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. This combines with the similitude to give a piston theo...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
The Jangjeon Mathematical Society (JMS)
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49812/1/asha-crasta.pdf |
| _version_ | 1825649570238955520 |
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| author | Khan, Sher Afghan Crasta , Asha |
| author_facet | Khan, Sher Afghan Crasta , Asha |
| author_sort | Khan, Sher Afghan |
| collection | IIUM |
| description | In the present study Supersonic similitude has been used
to obtain stability derivatives in pitch and roll of a delta wing for the
attached shock case. A strip theory is used in which strips at different
span-wise locations are independent. This combines with the similitude
to give a piston theory. The present theory is valid only for attached
shock case. Effects of wave re
ection and viscosity have not been taken
into account. Some of the results have been compared with those of Hui
et al (1982), Ghosh (1984), and Liu and Hui (1977). Results have been
obtained for supersonic
ow of perfect gas over a wide range of Mach
numbers, incidences and sweep angles. A good agreement is obtained
with Hui et al in some special cases. |
| first_indexed | 2024-03-05T23:49:30Z |
| format | Article |
| id | oai:generic.eprints.org:49812 |
| institution | International Islamic University Malaysia |
| language | English |
| last_indexed | 2024-03-05T23:49:30Z |
| publishDate | 2010 |
| publisher | The Jangjeon Mathematical Society (JMS) |
| record_format | dspace |
| spelling | oai:generic.eprints.org:498122016-07-18T07:56:52Z http://irep.iium.edu.my/49812/ Oscillating supersonic delta wings with curved leading edges Khan, Sher Afghan Crasta , Asha QA75 Electronic computers. Computer science In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. This combines with the similitude to give a piston theory. The present theory is valid only for attached shock case. Effects of wave re ection and viscosity have not been taken into account. Some of the results have been compared with those of Hui et al (1982), Ghosh (1984), and Liu and Hui (1977). Results have been obtained for supersonic ow of perfect gas over a wide range of Mach numbers, incidences and sweep angles. A good agreement is obtained with Hui et al in some special cases. The Jangjeon Mathematical Society (JMS) 2010-07 Article PeerReviewed application/pdf en http://irep.iium.edu.my/49812/1/asha-crasta.pdf Khan, Sher Afghan and Crasta , Asha (2010) Oscillating supersonic delta wings with curved leading edges. Advanced Studies in Contemporary Mathematics, 20 (3). pp. 359-372. ISSN 1229-3067 http://www.jangjeon.or.kr/etc/Search.html?division=ASCM&year=2010 |
| spellingShingle | QA75 Electronic computers. Computer science Khan, Sher Afghan Crasta , Asha Oscillating supersonic delta wings with curved leading edges |
| title | Oscillating supersonic delta wings with curved leading edges |
| title_full | Oscillating supersonic delta wings with curved leading edges |
| title_fullStr | Oscillating supersonic delta wings with curved leading edges |
| title_full_unstemmed | Oscillating supersonic delta wings with curved leading edges |
| title_short | Oscillating supersonic delta wings with curved leading edges |
| title_sort | oscillating supersonic delta wings with curved leading edges |
| topic | QA75 Electronic computers. Computer science |
| url | http://irep.iium.edu.my/49812/1/asha-crasta.pdf |
| work_keys_str_mv | AT khansherafghan oscillatingsupersonicdeltawingswithcurvedleadingedges AT crastaasha oscillatingsupersonicdeltawingswithcurvedleadingedges |