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On the hypersonic sharp leading edge problem for bodies other than flat plates

by Soloman, Jay M | .

Series: BSI 6737 : 1986Edition: Language: English Publication details: White Oak ; U.S. Naval Ordnance Laboratory, ; 1965Availability: Items available for loan: 1 Call number: 533.6.011 Sol.

Development of a device for controlling the leading edge vortices on a delta wing

by Gad-el-Hak, Mohamed | .

Series: Edition: Language: English Publication details: ; Kent : Flow Research, 1986 ; 1986Availability: Items available for loan: 1 Call number: 533.693 Gad.

Analysis of wings with leading edge and/or trailing edge segmented (spanwise) flaps using planar horse shoe vortex-lattic method

by Rajeshwari, B | Dutt, H.N.V | .

Series: Edition: Language: English Publication details: Bangalore ; National Aeronautical Lab., ; 1985Availability: Items available for loan: 1 Call number: 533.692 Raj.

Passive control of flow oscillations in a rectangular cavity using leading edge mounted tabs (R)

by Narayanan, A. Sathia | Sharma, S.D [Superviosr] | Venkatakrishnan, L [Supervisor] | Indian Institute of Technology Bombay Department of Aerospace Engineering.

Material type: Text Text; Format: print ; Literary form: Not fiction Language: English Publication details: Bombay IIT 2019Dissertation note: Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aerospace Engineering 2019 Availability: Items available for reference: Not for loan (1) Call number: 043:533.6.01 Nar.

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