Výsledky vyhledávání - "Kevin D. James"

Estimating Flow-Through Balance Momentum Tares with CFD (Invited)

Autor: Jeff D. Flamm, Kurtis R. Long, John E. Melton, Kevin D. James

Publikováno v: 54th AIAA Aerospace Sciences Meeting.

This paper describes the process used for estimating flow-through balance momentum tares. The interaction of jet engine exhausts on the BOEING/ERA Hybrid Wing Body (HWB) was simulated in the NFAC 40x80 wind tunnel at NASA Ames using a pair of turbine

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::52b2475864c82556a89c9e7d27dd49df
https://doi.org/10.2514/6.2016-0265

Zobrazit plný text záznamu

NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration (Invited)

Autor: James M. Luckring, Ben Nikaido, Joseph A. Garcia, Robert Childs, Dan D. Vicroy, Melissa B. Carter, Michael J. Schuh, Paul Stremel, Jeffrey D. Flamm, Karen A. Deere, Kevin D. James, John E. Melton, Kurtis R. Long

Publikováno v: 54th AIAA Aerospace Sciences Meeting.

NASAs Environmentally Responsible Aviation (ERA) Project explores enabling technologies to reduce aviations impact on the environment. One research challenge area for the project has been to study advanced airframe and engine integration concepts to

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::334469dff0999c37ba68109a4dd36014
https://doi.org/10.2514/6.2016-0262

Zobrazit plný text záznamu

Experimental Evaluation of Inlet Distortion on an Ejector Powered Hybrid Wing Body at Take-off and Landing Conditions (Invited)

Autor: Michael J. Schuh, Jeffrey D. Flamm, Daniel M. Tompkins, Patrick R. Shea, Matthew R. Sexton, Melissa B. Carter, Kevin D. James, Michael D. Beyar

Publikováno v: 54th AIAA Aerospace Sciences Meeting.

Due to the aft, upper surface engine location on the Hybrid Wing Body (HWB) planform, there is potential to shed vorticity and separated wakes into the engine when the vehicle is operated at off-design conditions and corners of the envelope required

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::388b52229314a2657e23dd04723ca2eb
https://doi.org/10.2514/6.2016-0010

Zobrazit plný text záznamu

Overview Of ERA Integrated Technology Demonstration (ITD) 51A Ultra-High Bypass (UHB) Integration for Hybrid Wing Body (HWB) (Invited)

Autor: John T. Bonet, Kevin D. James, Jeffrey D. Flamm

Publikováno v: 54th AIAA Aerospace Sciences Meeting.

The NASA Environmentally Responsible Aircraft Project (ERA) was a ve year project broken into two phases. In phase II, high N+2 Technical Readiness Level demonstrations were grouped into Integrated Technology Demonstrations (ITD). This paper describe

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5c096f314dd02763591e4eadbfef0d33
https://doi.org/10.2514/6.2016-0007

Zobrazit plný text záznamu

Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration (Invited)

Autor: Patrick R. Shea, Kevin D. James, Michael D. Beyar, Jeffrey D. Flamm, Kurtis R. Long, Daniel M. Tompkins

Publikováno v: 54th AIAA Aerospace Sciences Meeting.

Propulsion airframe integration testing on a 5.75% scale hybrid wing body model us- ing turbine powered simulators was completed at the National Full-Scale Aerodynamics Complex 40- by 80-foot test section. Four rear control surface con gurations incl

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::26365de63f5895bf965481e293a228b6
https://doi.org/10.2514/6.2016-0011

Zobrazit plný text záznamu

Full-scale wind-tunnel studies of F/A-18 tail buffet

Autor: Kevin D. James, Larry A. Meyn

Publikováno v: Journal of Aircraft. 33:589-595

Tail buffet studies were conducted on a full-scale, production F/A-18 fighter aircraft in the 80 by 120 ft Wind Tunnel at NASA Ames Research Center. The F/A-18 was tested over an angle-of-attack range of 18-50 deg, and at wind speeds of up to 168 ft/

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::df7dad9ebfe973be901c2c73f8f9b5ea
https://doi.org/10.2514/3.46986

Zobrazit plný text záznamu

Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80 Foot Wind Tunnel

Autor: Paul T. Soderman, Kevin D. James, Steven Jaeger, Thomas K. Arledge, Nathan J. Burnside, William C. Horne

Publikováno v: 11th AIAA/CEAS Aeroacoustics Conference.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7e0c7618254f67ae2d750459c085a0c2
https://doi.org/10.2514/6.2005-2810

Zobrazit plný text záznamu

Microphone Array Assessment of an Isolated, 26%-scale, High-fidelity Landing Gear

Autor: W. Clifton Horne, Stephen M. Jaeger, Nathan J. Burnside, Paul T. Soderman, Kevin D. James

Publikováno v: 8th AIAA/CEAS Aeroacoustics Conference & Exhibit.

An aeroacoustic study of a 26%-scale landing gear model was conducted in the NASA Ames 7- by 10-Foot Wind Tunnel using a phased microphone array. The incorporation of complex parts via stereo lithography produced a model that can mimic full-scale det

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::786683c4a4dd93e5222e9e7b4b9f8878
https://doi.org/10.2514/6.2002-2410

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání