Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Eric J. Gamble"'
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A jet noise prediction tool has been developed for predicting jet noise and for performing system level trade studies within propulsion system analyses. This tool, NozzleDB, incorporates Jet3D, a RANS-based jet noise prediction scheme based on Lighth
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A dynamic simulator is being developed to demonstrate all modes of operation, including mode transition, for a Turbine-Based Combined Cycle (TBCC) propulsion system. The High Mach Transient Engine Cycle Code (HiTECC) is a highly integrated simulation
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A Scramjet/Ramjet Heat Exchanger Analysis Tool (SRHEAT) has been developed for rapid analyses of complex thermal cooling systems. The detailed heat exchanger design features included in this code (i.e. geometry, material properties, fuel/coolant prop
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
A user-friendly heat transfer/thermal modeling code, LinerTherm, has been developed for rapid analysis of aircraft exhaust liner cooling systems. Most of the thermal modeling codes on the market today fall into one of two categories either they are c
Publikováno v:
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Autor:
Eric J. Gamble, Dan Haid
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
I. ABSTRACT High transonic drag is an issue that must be considered in the design of supersonic vehicles. Generally, aftbody drag is greatest at flight Mach numbers near 1.0. This study has shown numerically that fluidic injection can be used to decr
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Advances in aircraft performance depend heavily upon improved and properly integrated propulsion systems. Historically, new engines and aircraft are developed concurrently, but the design and test cycle of engine systems is longer than that of the ai
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
A test was conducted to measure the time-averaged flow rate of a pulse detonation engine. The objective of this flow test was to determine the flow effectiveness of a pulse detonation engine utilizing a rotating spool of tubes. Since thrust is direct
Autor:
Dan Haid, Eric J. Gamble
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.