Zobrazeno 1 - 7
of 7
pro vyhledávání: '"John D. Mcminn"'
Publikováno v:
Journal of Aircraft. 32:355-362
Many air-breathing hypersonic vehicle design concepts utilize the lower surface of an elongated fuselage forebody to provide aerodynamic compression for a supersonic combustion ramjet module, or a scramjet. This highly integrated design approach crea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1fd60895c91f46ab8a6a5d7a7004bef
https://doi.org/10.2514/3.46723
https://doi.org/10.2514/3.46723
Publikováno v:
AIAA Modeling and Simulation Technologies Conference and Exhibit.
An independent twelve degree-of-freedom simulation of the X-43A separation trajectory was created with the Program to Optimize Simulated trajectories (POST II). This simulation modeled the multi-body dynamics of the X-43A and its booster and included
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17b75bd2e6df9b9b69b0a450daf0256a
https://doi.org/10.2514/6.2003-5819
https://doi.org/10.2514/6.2003-5819
Autor:
D Bose, Mark Stephenson, John G. Martin, J Pahle, J Selmon, Jr J. Davidson, John D. Mcminn, F Lallman
Publikováno v:
Guidance, Navigation, and Control Conference and Exhibit.
The goal of the Hyper-X program is to demonstrate and validate technology for design and performance predictions of hypersonic aircraft with an airframe-integrated supersonic-combustion ramjet propulsion system. Accomplishing this goal requires fligh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::581bbdb32ad69a595ba9cf5fffd23bcc
https://doi.org/10.2514/6.1999-4124
https://doi.org/10.2514/6.1999-4124
Publikováno v:
34th Structures, Structural Dynamics and Materials Conference.
Many air-breathing hypersonic aerospacecraft design concepts incorporate an elongated fuselage forebody acting as the aerodynamic compression surface for a hypersonic combustion module, or scram jet. This highly integrated design approach creates the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::694e061b02fee6ff1c5a6546ddda5e63
https://doi.org/10.2514/6.1993-1367
https://doi.org/10.2514/6.1993-1367
Publikováno v:
AlAA 4th International Aerospace Planes Conference.
Applicability and effectivness of robust control techniques to a single-stage-to-orbit (SSTO) airbreathing hypersonic vehicle on an ascent accelerating path and their effectivness are explored in this paper. An SSTO control system design problem, req
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f40200fcb5b694eee16a3903a02d9ee1
https://doi.org/10.2514/6.1992-5010
https://doi.org/10.2514/6.1992-5010
Publikováno v:
30th Aerospace Sciences Meeting and Exhibit.
An atmospheric disturbance model (ADM) is developed that considers the requirements of advanced aerospace vehicles and balances algorithmic assumptions with computational constraints. The requirements for an ADM include a realistic power spectrum, in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a928bfdd908bb1a4cdcda98879769886
https://doi.org/10.2514/6.1992-294
https://doi.org/10.2514/6.1992-294
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