Investigation of the longitudinal stability at high speeds of a 1/5-scale model of a tailless pursuit airplane / by Edmund V. Laitone.
Tests of a tailless pursuit airplane model at the Ames Aeronautical Laboratory have shown that in conditions corresponding to level flight at a Mach number less than 0.7 and at an altitude under 35,000 feet, no serious compressibility effects occurred and that no sudden adverse diving moments were e...
Saved in:
| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series A. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1943]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. A77. |
| Subjects: |
MARC
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| 100 | 1 | |a Laitone, Edmund V. |0 http://id.loc.gov/authorities/names/no2014155607. | |
| 245 | 1 | 0 | |a Investigation of the longitudinal stability at high speeds of a 1/5-scale model of a tailless pursuit airplane / |c by Edmund V. Laitone. |
| 246 | 3 | |a NACA Wartime Reports. Series A. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1943] | ||
| 300 | |a 4 pages, 19 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. A77. | |
| 500 | |a NACA Wartime Report A-77. | ||
| 500 | |a Originally issued as NACA as a Memorandum Report (March 1943) | ||
| 500 | |a Prepared at the Ames Aeronautical Laboratory, Moffett Field, California. | ||
| 520 | 3 | |a Tests of a tailless pursuit airplane model at the Ames Aeronautical Laboratory have shown that in conditions corresponding to level flight at a Mach number less than 0.7 and at an altitude under 35,000 feet, no serious compressibility effects occurred and that no sudden adverse diving moments were encountered up to a Mach number of 0.74, the maximum speed of the tests. However, there were indications that the elevons might lose their effectiveness for longitudinal control during a pull-out from a steep dive. | |
| 650 | 0 | |a Fighter planes. |0 http://id.loc.gov/authorities/subjects/sh85048159. | |
| 650 | 0 | |a Tailless airplanes. |0 http://id.loc.gov/authorities/subjects/sh85002953. | |
| 650 | 0 | |a Stability of airplanes, Longitudinal. |0 http://id.loc.gov/authorities/subjects/sh85127188. | |
| 650 | 0 | |a Airplanes |x Handling characteristics. |0 http://id.loc.gov/authorities/subjects/sh85002825. | |
| 650 | 0 | |a Airplanes |x Models. |0 http://id.loc.gov/authorities/subjects/sh85002841. | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292. | |
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| 650 | 7 | |a Airplanes |x Models. |2 fast |0 (OCoLC)fst00803299. | |
| 650 | 7 | |a Tailless airplanes. |2 fast |0 (OCoLC)fst00803672. | |
| 650 | 7 | |a Fighter planes. |2 fast |0 (OCoLC)fst00923996. | |
| 650 | 7 | |a Stability of airplanes, Longitudinal. |2 fast |0 (OCoLC)fst01131217. | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
| 710 | 2 | |a Ames Research Center. |0 http://id.loc.gov/authorities/names/n79138699 |1 http://isni.org/isni/0000000119557990. | |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. A77. | |
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