Zobrazeno 1 - 10
of 53
pro vyhledávání: '"Paul Weinacht"'
Publikováno v:
Shock and Vibration, Vol 10, Iss 2, Pp 115-126 (2003)
An effort to improve the performance of ordnance has led to the consideration of the use of folding elliptical fins for projectile stabilization. A second order differential equation was used to model elliptical fin deployment history and accounts fo
Externí odkaz:
https://doaj.org/article/54b3e66b52a44a388c7ced8e8a5df946
Autor:
Paul Weinacht, James E. Danberg
Publikováno v:
Journal of Spacecraft and Rockets. 42:865-872
Throughout its development, slender body theory has been generalized to predict a large variety of aerodynamic coefficients for a wide class of flight bodies. For most applications, slender body theory provides only a qualitative predictive capabilit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f4eb0a6a6b8103032f0c6ec209e64417
https://doi.org/10.2514/1.10718
https://doi.org/10.2514/1.10718
Autor:
Paul Weinacht
Publikováno v:
Journal of Spacecraft and Rockets. 41:257-263
With the recent development of capabilities for predicting damping derivatives, it is now possible to predict the stability characteristics and free-flight motion for projectiles using data that are derived solely from computational fluid dynamics (C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21519f1aba9c557e04a5b1d18564b654
https://doi.org/10.2514/1.1037
https://doi.org/10.2514/1.1037
Publikováno v:
Journal of Spacecraft and Rockets. 39:376-383
A detailed numerical investigation of the interaction between a lateral jet and the external flow has been performed for a variety of missile body geometries. These include non-finned axisymmetrical bodies and finned bodies with either strakes or aft
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::347eb3a1bb1bbd3647227cbc4f672284
https://doi.org/10.2514/2.3836
https://doi.org/10.2514/2.3836
Publikováno v:
Defence Science Journal. 52:77-85
The influence of quasi-independent parameters and their potential influence on erosion in guns have been investigated. Specifically, the effects of flame temperature and the effect of assuming that the Lewis number (ratio of mass-to-heat transport to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a5f9f0796c827230bb5baec5ffd9f3a
https://doi.org/10.14429/dsj.52.2152
https://doi.org/10.14429/dsj.52.2152
Autor:
Paul Weinacht
This report presents a simple but accurate method of determining the trajectory of projectiles that traverse a flight regime that includes supersonic, transonic, and subsonic flight. Closed-form analytical solutions for the important trajectory param
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e24b5c44a2ee67a69c29cd2f1661540
https://doi.org/10.21236/ada607593
https://doi.org/10.21236/ada607593
Publikováno v:
Journal of Spacecraft and Rockets. 38:711-718
An approach for using viscous computational e uid dynamic simulations to calculate the e owe eld and aerodynamic coefe cients for a missile with grid e ns is presented. A grid e n is an unconventional lifting and control surfacethatconsists of an out
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a930294c96f5fedf06ff56a30a4c704f
https://doi.org/10.2514/2.3756
https://doi.org/10.2514/2.3756
Autor:
Paul Weinacht, Mary Jane Graham
Publikováno v:
Journal of Spacecraft and Rockets. 37:675-683
A detailed numerical investigation of the interaction between a lateral jet and the external e ow has been performed for several axisymmetric bodies. Numerical predictions of the supersonic viscous e ow has been obtained using an existing Reynolds-av
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::361648f77d37621d9471625ade4041da
https://doi.org/10.2514/2.3617
https://doi.org/10.2514/2.3617
Publikováno v:
Journal of Spacecraft and Rockets. 37:257-264
Experimentaland engineering modelingtechniqueswereapplied toexaminetherolethatelectromagneticsplays duringthesabotdiscardprocessina solid-armaturerailgun.Currentandmagnetice elddiffusionintheconducting armature and sabot produce residual forces that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f90413abfc69bb642c8b6db9bd9f5596
https://doi.org/10.2514/2.3554
https://doi.org/10.2514/2.3554
Autor:
Paul Weinacht
Publikováno v:
Journal of Spacecraft and Rockets. 35:598-605
An approach for predicting the two individual aerodynamic damping coefe cients that form the pitch-damping coefe cient sum is presented. The coefe cients are obtained using prescribed or forced motions that independently excite the two different angu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38595cd35b2ba46dc7f5129d759b27a4
https://doi.org/10.2514/2.3390
https://doi.org/10.2514/2.3390