Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Donald Freund"'
Autor:
Donald Freund, Miklos Sajben
Publikováno v:
Journal of Propulsion and Power. 16:406-414
The reliability of unsteady inlet e ow computations may be seriously degraded by the lack of experimentally validated compressor-face (outeow) boundary conditions. The commonly imposed oute ow conditions require a e ow variableto beconstant (pressure
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7bd834aa80e77850a48243a9254a3d41
https://doi.org/10.2514/2.5604
https://doi.org/10.2514/2.5604
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3582e2c9c336f38772416bc1ea99a9b8
https://doi.org/10.2514/6.2008-127
https://doi.org/10.2514/6.2008-127
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
The Quiet Spike is a concept developed by Gulfstream Aerospace Corporation that breaks up the sonic boom generated by an aircraft traveling at supersonic speeds. The concept employs a structural boom that extends forward from the fuselage. Spaced alo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1f70b25637d504d85b24645546bfcab6
https://doi.org/10.2514/6.2008-125
https://doi.org/10.2514/6.2008-125
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
The Gulfstream Quiet Spike is a telescoping forward fuselage extension that alters the bow shock of the classic N-wave pressure signature generated by aircraft traveling at supersonic speeds. The bow shock is broken up into sequence of weak shocks th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5164893d4876b9bf3a9a4f9bb2965d30
https://doi.org/10.2514/6.2008-124
https://doi.org/10.2514/6.2008-124
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
†∗ + # Gulfstream and NASA Dryden recently completed flight testing the Quiet Spike™ installed on Dryden’s F-15B research test bed aircraft. The Quiet Spike is a segmented, telescoping nose boom that increases the aircraft overall length for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::26e0bdb7671a2b30902e1fc59b611bfc
https://doi.org/10.2514/6.2007-1778
https://doi.org/10.2514/6.2007-1778
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4210c1dce694e964631b09dbed0ebba7
https://doi.org/10.2514/6.2007-1774
https://doi.org/10.2514/6.2007-1774
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
NASA's Dryden Flight Research Center uses a modified F-15B (836) aircraft as a testbed for a variety of flight research:experiments mounted underneath the aircraft fuselage. The F-15B was selected to fly Gulfstream Aerospace Corporation's (GAC)QuietS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d280ef10c4edcb0a0672c2ef6039e1ad
https://doi.org/10.2514/6.2007-1775
https://doi.org/10.2514/6.2007-1775
Autor:
Frank Simmons, Donald Freund
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
In order for a supersonic business jet to be economically viable, it must perform to several stringent criteria. The ability to travel over land supersonically and to operate in general airports that already are extensively used by subsonic business
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::934468cb33dd1ba16745d533ce91ce0c
https://doi.org/10.2514/6.2005-1017
https://doi.org/10.2514/6.2005-1017
Autor:
Donald Freund, Frank Simmons
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
A morphing concept for a Quiet Supersonic Jet (QSJ) is presented that produces a shaped sonic boom with very low initial overpressure. Morphing of the aircraft involves lengthening the fuselage via an extendable nose spike. The extendable nose spike
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc851e743e7dc7412c7b1b409802231e
https://doi.org/10.2514/6.2005-1015
https://doi.org/10.2514/6.2005-1015
Publikováno v:
41st Structures, Structural Dynamics, and Materials Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07036d59895a708b98a9ba6ce268bc75
https://doi.org/10.2514/6.2000-1526
https://doi.org/10.2514/6.2000-1526