The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps
This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civil...
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Pasadena, California; California Institute of Technology
2012
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Online Access: | http://hdl.handle.net/10945/6379 |
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ndltd-nps.edu-oai-calhoun.nps.edu-10945-63792015-05-06T03:57:52Z The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps Weitzenfeld, Daniel K. Trauger, Robert J. Kronmiller, George R. Liepmann, Hans. W. California Institute of Technology Department of Aeronautics This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title. It was desired in this investigation to determine the effect of the chordwise position of dive recovery flaps on the left of a laminar flow, low drag, two-dimensional airfoil at high subsonic Mach numbers. Schieren pictures were taken to relate the formation, extension and strength of shock waves to the measured lift. 2012-03-14T17:52:17Z 2012-03-14T17:52:17Z 1946-06 Thesis http://hdl.handle.net/10945/6379 en_US Pasadena, California; California Institute of Technology |
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NDLTD |
language |
en_US |
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NDLTD |
description |
This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title. === It was desired in this investigation to determine the effect of the chordwise position of dive recovery flaps on the left of a laminar flow, low drag, two-dimensional airfoil at high subsonic Mach numbers. Schieren pictures were taken to relate the formation, extension and strength of shock waves to the measured lift. |
author2 |
Liepmann, Hans. W. |
author_facet |
Liepmann, Hans. W. Weitzenfeld, Daniel K. Trauger, Robert J. Kronmiller, George R. |
author |
Weitzenfeld, Daniel K. Trauger, Robert J. Kronmiller, George R. |
spellingShingle |
Weitzenfeld, Daniel K. Trauger, Robert J. Kronmiller, George R. The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
author_sort |
Weitzenfeld, Daniel K. |
title |
The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
title_short |
The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
title_full |
The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
title_fullStr |
The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
title_full_unstemmed |
The effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
title_sort |
effect of dive recovery flaps on the lift of a two dimensional symmetrical airfoil with changes in chordwise location of the flaps |
publisher |
Pasadena, California; California Institute of Technology |
publishDate |
2012 |
url |
http://hdl.handle.net/10945/6379 |
work_keys_str_mv |
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