Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap / by Eastman N. Jacobs.
The general problem of stalling as affecting the safety of airplanes is considered. The increased difficulties associated with modern efficient wings, particularly with highly tapered wings and high-lift devices, are discussed and various means are considered of avoiding these difficulties with a mi...
Saved in:
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1937]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L296. |
| Subjects: |
MARC
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| 100 | 1 | |a Jacobs, Eastman N. |q (Eastman Nixon), |d 1902-1987 |0 http://id.loc.gov/authorities/names/no2008029956. | |
| 245 | 1 | 0 | |a Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap / |c by Eastman N. Jacobs. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1937] | ||
| 300 | |a 17 pages, 9 unnumbered pages : |b illustrations ; |c 27 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 Wartime Report / National Advisory Committee for Aeronautics ; |v no. L296. | |
| 500 | |a NACA Wartime Report L-296. | ||
| 500 | |a Originally issued as NACA as an Advance Confidential Report (November 1937) | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a The general problem of stalling as affecting the safety of airplanes is considered. The increased difficulties associated with modern efficient wings, particularly with highly tapered wings and high-lift devices, are discussed and various means are considered of avoiding these difficulties with a minimum aerodynamic loss. Finally, preliminary data are presented for the stall-control flap and the application of these section data to wing design is briefly covered, mainly by means of an example. | |
| 650 | 0 | |a Airplanes |x Wings. |0 http://id.loc.gov/authorities/subjects/sh85002923. | |
| 650 | 0 | |a Airplanes |x Control. | |
| 650 | 0 | |a Flaps (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85049001. | |
| 650 | 0 | |a Stalling (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85127283. | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292. | |
| 650 | 0 | |a Charts, diagrams, etc. |0 http://id.loc.gov/authorities/subjects/sh87002373. | |
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| 650 | 7 | |a Airplanes |x Wings. |2 fast |0 (OCoLC)fst00803545. | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545. | |
| 650 | 7 | |a Flaps (Airplanes) |2 fast |0 (OCoLC)fst00927038. | |
| 650 | 7 | |a Stalling (Aerodynamics) |2 fast |0 (OCoLC)fst01131402. | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047. | |
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| 710 | 2 | |a Langley Aeronautical Laboratory. |0 http://id.loc.gov/authorities/names/n81018841. | |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L296. | |
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