A note on the aerodynamic design of thin parallel-sided aerofoil-sections (U) / by N. Pollock
- Bib ID:
- 680180
- Format:
- Book
- Author:
- Pollock, N
- Description:
-
- Melbourne : Dept. of Defence, Defence Science and Technology Organisation, Aeronautical Research Laboratories, 1987
- 9, 13 leaves : ill. ; 30 cm.
- ISBN:
- 0642132933
- Series:
- Aerodynamics technical memorandum ; 388.
- Summary:
-
There are many situations where parallel-sided aerofoil sections with leading and trailing edge fairings of limited chordwise extent have advantages over conventional sections. The design of these unconventional sections was investigated using two potential flow plus boundary layer computer programs. Guidelines for the selection of the leading and trailing edge fairing shapes are presented.
- Notes:
- AR-004-551.
- Subject:
- Aerofoils -- Design and construction
- Other authors/contributors:
- Aeronautical Research Laboratories (Australia)
- Terms of Use:
- Commonwealth of Australia 1987.
- Copyright:
-
In Copyright
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- Reason for copyright status:
- Until 2037 [Created/Published Date + 50 Years]
Copyright status was determined using the following information:
- Material type:
- Literary Dramatic Musical
- Published status:
- Published
- Publication date:
- 1987
Copyright status may not be correct if data in the record is incomplete or inaccurate. Other access conditions may also apply. For more information please see: Copyright in library collections.
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