Zobrazeno 1 - 10
of 38
pro vyhledávání: '"G. Lengelle"'
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 5:90-100
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::35ac8112d9f3593f4c245c6b4f52c007
https://doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.130
https://doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.130
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 5:699-711
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9cc787d8fcd43289dd456a315bb8466b
https://doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.720
https://doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.720
Autor:
G. Lengelle
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 4:515-548
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c3d1c1ef1484ebe96c14b85210e46a4
https://doi.org/10.1615/intjenergeticmaterialschemprop.v4.i1-6.510
https://doi.org/10.1615/intjenergeticmaterialschemprop.v4.i1-6.510
Publikováno v:
Journal of Propulsion and Power. 8:741-747
A modeling approach based on experimental verification for the erosive burning of ammonium perchlorate composite propellants is proposed. It retains the idea that erosive burning is due to the penetration of the flow turbulence within the flame heigh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc5abeed56d7a492bdf7c6126a622717
https://doi.org/10.2514/3.23544
https://doi.org/10.2514/3.23544
Autor:
G. Lengelle, Jean Duterque
Publikováno v:
Journal of Propulsion and Power. 6:718-726
Propellants containing HMX and an energetic binder have a very pressure sensitive burning rate law. Modifications of the burning rate and of the pressure exponent may be obtained by adding lead salts or ammonium perchlorate (AP) to the propellant. In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10ea5b4b2465eeb0cda2ccce003e2b42
https://doi.org/10.2514/3.23277
https://doi.org/10.2514/3.23277
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06515cf116df632ab1e98ceb4cb3779e
https://doi.org/10.2514/6.1999-2321
https://doi.org/10.2514/6.1999-2321
Publikováno v:
29th Joint Propulsion Conference and Exhibit.
The regression rate of a fuel for hybrid propulsion applications results from the coupling between the heat flux density issuing from the reacting cross {Jow and the energy required by the condensed phase process. Three fuels are considered polyethyl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e60cb0cd0c96aa3895fc3d03a4224ab0
https://doi.org/10.2514/6.1993-2413
https://doi.org/10.2514/6.1993-2413
Publikováno v:
Symposium (International) on Combustion. 16:1257-1269
By means of theoretical modeling as well as by the experimental investigation of various propellants, further elements are presented to consolidate the understanding of the combustion of ammonium perchlorate propellants. Available descriptions of A.P
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::981d5ff95aa037742d80f618931df93b
https://doi.org/10.1016/s0082-0784(77)80413-x
https://doi.org/10.1016/s0082-0784(77)80413-x
Publikováno v:
Propellants, Explosives, Pyrotechnics. 10:18-25
Experimental results about rb(P) laws of double-base propellants are presented. The influence of many parameters (calorific potential, fabrication process, additives) is studied. With surface structure examination, we show that the first super-rate (
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::efb16a6c9f1ed8ba1616d46a9b3234bc
https://doi.org/10.1002/prep.19850100106
https://doi.org/10.1002/prep.19850100106
Autor:
G. Lengelle
Publikováno v:
AIAA Journal. 13:315-322
A detailed model is presented which permits one to represent the response of the burning rate of an ammonium perchlorate solid composite propellant to pressure and velocity fluctuations. First, the steady regime response of the burning velocity of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46bf7731412edd2aa7a73696bf98622e
https://doi.org/10.2514/3.49697
https://doi.org/10.2514/3.49697