Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Wallace Chinitz"'
Publikováno v:
Journal of Propulsion and Power. 28:412-422
To counter the extreme heat loads experienced by hypersonic engine structures, it is imperative that fuels double as coolants. However, the use of logistical fuels (e.g., JP-7 and JP-10) in hypersonic applications is becoming more accepted in near-te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4b0f8e1aa7805313cb9462ef7b03d23c
https://doi.org/10.2514/1.b34118
https://doi.org/10.2514/1.b34118
Publikováno v:
Journal of Propulsion and Power. 28:412-422
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e19f85651fdf4ba81b88d90f66e9cf59
https://doi.org/10.2514/1.57815
https://doi.org/10.2514/1.57815
Publikováno v:
Journal of Propulsion and Power. 10:6-17
Wallace Chinitz is a Principal Scientist at General Applied Science Laboratories (GASL) as well as a Professor of Mechanical Engineering at Cooper Union's Nerken School of Engineering. He received his Ph.D. from the Polytechnic Institute of Brooklyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::427c7cd51ddb1ed16c7304f64d130329
https://doi.org/10.2514/3.23705
https://doi.org/10.2514/3.23705
Publikováno v:
Journal of Propulsion and Power. 9:731-738
The feasibility of a Mach 10 to 20, high pressure electrothermal wind tunnel was assessed. A heater based on a continuous high power electric arc discharge capable of heating air to temperatures above 10,000 K and pressures of 15,000 atm is the key e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9df4421ce7931f0ec5b2ace91b9aade
https://doi.org/10.2514/3.23683
https://doi.org/10.2514/3.23683
Continued Investigation of Short Contact Time Reactors for Regeneratively-Cooled Hypersonic Vehicles
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::97a5ef5ccff97c7c1260d7a29e2a4dd4
https://doi.org/10.2514/6.2010-6791
https://doi.org/10.2514/6.2010-6791
Publikováno v:
Journal of Propulsion and Power. 8:1290-1296
Testing at hypervelocity test conditions continues in the Hypulse expansion tube. A newly-calibrated Mach 13 operating point has been achieved, and hydrogen injection studies were performed at this test condition. The experiments were conducted in a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36d55ee7c940313d427f753cc55d1705
https://doi.org/10.2514/3.11475
https://doi.org/10.2514/3.11475
Publikováno v:
Journal of Propulsion and Power. 8:900-906
Hydrogen-air mixing and combustion experiments at air velocities approaching 17,000 ft/s have been conducted in the HYPULSE facility expansion tube. The results proved to be repeatable and indicated increasing extent of reaction as the fuel equivalen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::afe4b528d00e8d014bb90661a6357419
https://doi.org/10.2514/3.23567
https://doi.org/10.2514/3.23567
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Scramjet engines have long been considered potential propulsion systems for lowcost access to lowEarth orbit, as well as longrange intercontinental flights. For this concept to be viable, however, additional work is necessary in designing engin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e481486de7e68531fd856f505eb621ed
https://doi.org/10.2514/6.2006-4403
https://doi.org/10.2514/6.2006-4403
Publikováno v:
20th AIAA Advanced Measurement and Ground Testing Technology Conference.
Details on the design, fabrication and calibration of a nominal Mach 6.5 hypersonic shock tunnel nozzle are presented. The nozzle design intent, nozzle-facility interface, material selection, and chosen method of construction are also reviewed. Flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ca7ab843b8a725e8dacda1b5d9d9fc4
https://doi.org/10.2514/6.1998-2496
https://doi.org/10.2514/6.1998-2496
Autor:
Wallace Chinitz
Publikováno v:
Space Plane and Hypersonic Systems and Technology Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c52a2636f3b23c95a6b23634082577d
https://doi.org/10.2514/6.1996-4536
https://doi.org/10.2514/6.1996-4536