Zobrazeno 1 - 10
of 84
pro vyhledávání: '"ADAM P. BRUCKNER"'
Publikováno v:
AIAA Scitech 2021 Forum.
Publikováno v:
Applied Spectroscopy. 74:160-167
Results and analysis of internal reflection spectral absorbance experiments are reported for near-infrared (NIR) spectra obtained using an optical fiber sensor system. We present a preliminary study to diagnose the efficacy of our fiber optic system
Publikováno v:
Aerotecnica Missili & Spazio. 97:19-26
Advances made to the unsteady, one-dimensional (1-D) modeling of the thermally choked ram accelerator thrust-Mach number characteristics include the use of real-gas equations of state to account for the compressibility effects of the combustion produ
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Autor:
Jonathan P. Lee, Adam P. Bruckner
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Autor:
Adam P. Bruckner, Carl Knowlen
Publikováno v:
Hypervelocity Launchers ISBN: 9783319260167
The ram accelerator, conceived at the University of Washington in 1983, is a scalable hypervelocity launcher, capable, in principle, of accelerating projectiles to velocities greater than 8 km/s. The device operates as an in-bore ramjet in which a su
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::596c59d93c1ba8e01489ea38a30b5265
https://doi.org/10.1007/978-3-319-26018-1_4
https://doi.org/10.1007/978-3-319-26018-1_4
Publikováno v:
Journal of Propulsion and Power. 21:955-958
A = tube section a = acceleration cp = isobaric heat capacity F = thrust h = specific enthalpy I = nondimensional thrust, F/(p A) L = length M = Mach number m = mass P = pressure ratio p = pressure Q = nondimensional heat release, q/cpT R = gas const
Publikováno v:
The European Physical Journal Applied Physics. 29:253-258
The predicted acceleration performance of the ram accelerator at elevated pressures, based on the quasi-steady model, is much greater than that observed in experiments. This discrepancy is attributed to the increase of mass of the propellant accumula
Publikováno v:
Le Journal de Physique IV. 10:Pr11-49
An experimental investigation of the effects of obturator geometry, propellant chemistry, and onboard pyrotechnic ignitor systems on the starting characteristics of the ram accelerator at low launch velocity has been conducted at the University of Wa