Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion

Bibliographic Details
Main Authors: Schuld, Emil P., Reinhart, Leonard J.
Language:en_US
Published: Princeton University 2012
Online Access:http://hdl.handle.net/10945/24662
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-246622014-11-28T03:59:23Z Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion Schuld, Emil P. Reinhart, Leonard J. 2012-12-26T23:07:47Z 2012-12-26T23:07:47Z 1953-06 Thesis http://hdl.handle.net/10945/24662 ocn640257227 en_US Princeton University
collection NDLTD
language en_US
sources NDLTD
author Schuld, Emil P.
Reinhart, Leonard J.
spellingShingle Schuld, Emil P.
Reinhart, Leonard J.
Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
author_facet Schuld, Emil P.
Reinhart, Leonard J.
author_sort Schuld, Emil P.
title Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
title_short Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
title_full Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
title_fullStr Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
title_full_unstemmed Determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the Ryan Navion
title_sort determination of longitudinal stability parameters by steady state flight testing and theoretical calculations for the ryan navion
publisher Princeton University
publishDate 2012
url http://hdl.handle.net/10945/24662
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AT reinhartleonardj determinationoflongitudinalstabilityparametersbysteadystateflighttestingandtheoreticalcalculationsfortheryannavion
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