Lateral oscillations occurring on the aircraft model of NASA TP 1803 at angles of attack ranging from 25 ะ to 60 ะ have been investigated in a low-speed wind tunnel for configurations including fuselage with wing or with a combination of wing and leadingedge extension (LEX) . The wind tunnel experim
Non-linear stability analysis of aircraft at high angles of attack
โ Scribed by N.Sri Namachchivaya; S.T. Ariaratnam
- Book ID
- 103126958
- Publisher
- Elsevier Science
- Year
- 1986
- Tongue
- English
- Weight
- 829 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0020-7462
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