| Year |
Citation |
Score |
| 2015 |
Schrage DP. Value-driven rotorcraft design through integrated product/process development and robust design simulation 41st European Rotorcraft Forum 2015, Erf 2015. 1: 539-551. |
0.382 |
|
| 2014 |
Melnyk R, Schrage D, Volovoi V, Jimenez H. Sense and avoid requirements for unmanned aircraft systems using a target level of safety approach. Risk Analysis : An Official Publication of the Society For Risk Analysis. 34: 1894-906. PMID 24724619 DOI: 10.1111/Risa.12200 |
0.327 |
|
| 2013 |
Silva J, Schrage DP, Bauer N, Meng R, Wallace P. Evaluation of a Collaborative Aerospace Lifecycle Systems Engineering Master's Program Procedia Computer Science. 16: 957-966. DOI: 10.1016/J.Procs.2013.01.100 |
0.46 |
|
| 2013 |
Roberts MDP, Ashok SV, Sirirojvisuth A, Schrage DP. Design space exploration tool for future rotorcraft applications Annual Forum Proceedings - Ahs International. 3: 2030-2042. |
0.766 |
|
| 2013 |
Ashok SV, Schrage DP. Optimization techniques for gear train design Annual Forum Proceedings - Ahs International. 1: 449-467. |
0.303 |
|
| 2012 |
Ashok SV, Zender F, Sirirojvisuth A, Schrage DP. A method to integrate drive system design Annual Forum Proceedings - Ahs International. 4: 2377-2390. |
0.791 |
|
| 2012 |
Sirirojvisuth A, Schrage DP. Rotor blade manufacturing process tradeoffs using a cost/time analysis Annual Forum Proceedings - Ahs International. 3: 1921-1929. |
0.773 |
|
| 2012 |
Ashok SV, Sirirojvisuth A, Schrage DP. Systems engineering application for rotorcraft systems Annual Forum Proceedings - Ahs International. 4: 2722-2739. |
0.795 |
|
| 2011 |
Scott R, Schrage DP. Quantifying cost uncertainty effects of non-conventional systems on rotorcraft life cycle cost American Helicopter Society International - Technical Specialists' Meeting On Systems Engineering 2011. 142-159. |
0.331 |
|
| 2011 |
Ashok SV, Schrage DP, Robledo A. A systems engineering modeling and simulation approach for rotorcraft drive system optimization Annual Forum Proceedings - Ahs International. 4: 2885-2896. |
0.396 |
|
| 2011 |
Ashok SV, Sirirojvisuth A, Schrage DP. Drive system design integration for rotorcraft through Integrated Product-Process Development (IPPD) American Helicopter Society International - Technical Specialists' Meeting On Systems Engineering 2011. 256-286. |
0.797 |
|
| 2010 |
Schrage DP. Product Lifecycle Engineering (PLE): A manufacturing influenced design trade study application Annual Forum Proceedings - Ahs International. 1: 380-398. |
0.362 |
|
| 2009 |
Shrotri K, Schrage D. Composite skid landing gear performance and laminate tailoring for reduced load factor under limit loads Journal of the American Helicopter Society. 54. DOI: 10.4050/Jahs.54.042005 |
0.738 |
|
| 2009 |
Shrotri K, Schrage D. Composite skid landing gear design feasibility Journal of the American Helicopter Society. 54. DOI: 10.4050/Jahs.54.042004 |
0.77 |
|
| 2009 |
Moodie AM, Schrage DP, Sankar LN, Waters MH. Sizing and performance-prediction method for rotary-wing ejector nozzles Journal of Aircraft. 46: 951-961. DOI: 10.2514/1.39423 |
0.742 |
|
| 2007 |
Shrotri K, Manyapu K, Khalid A, Sumer YF, Gunduz ME, Schrage DP. Marvin- Near surface methane detection on mars Ieee Aerospace Conference Proceedings. DOI: 10.1109/AERO.2007.352714 |
0.683 |
|
| 2007 |
Jonnalagadda S, Sinha AK, Hoffmann P, Schauenburg A, Schrage DP. Modelling upgrade design analysis of maritime helicopters for anti-submarine missions-mission capability analysis National Aerospace Laboratory Nlr - 32nd European Rotorcraft Forum, Erf 2006. 2: 642-654. |
0.316 |
|
| 2007 |
Schrage DP, Suhr S, Sirirojvisuth A, Mishra SS. An IPPD approach for preliminary design of two-place turbine training helicopter Collection of Technical Papers - 2007 Aiaa Infotech At Aerospace Conference. 2: 1537-1558. |
0.781 |
|
| 2007 |
Khalid A, Schrage DP. Helicopter design cost minimization using multidisciplinary design optimization Annual Forum Proceedings - Ahs International. 3: 2103-2123. |
0.397 |
|
| 2007 |
Schrage DP, Volovoi V, Johnson E, Prasad JVR, Costello M. An integrated simulation and flight testing approach for Unmanned Aerial Systems (UAS) airworthiness criteria Ahs International Specialists' Meeting - Unmanned Rotorcraft: Design, Control and Testing. |
0.309 |
|
| 2007 |
Schrage DP. Integrated product and process development for the front end of rotorcraft systems engineering Annual Forum Proceedings - Ahs International. 3: 1640-1657. |
0.315 |
|
| 2006 |
Jonnalagadda S, Sinha AK, Hoffmann P, Schrage DP. A system framework of the design parametric analysis sub-module for modeling upgrade design analysis of anti-submarine maritime helicopters American Helicopter Society, Ahs Vertical Lift Design Conference. 2006: 355-362. |
0.321 |
|
| 2005 |
Jonnalagadda S, Sinha AK, Hoffmann P, Schrage DP. Modelling upgrade design analysis of maritime helicopters for anti-submarine missions - Mission payload design 31st European Rotorcraft Forum. 2005. |
0.362 |
|
| 2005 |
Jonnalagadda S, Sinha AK, Hoffmann P, Schrage DP. Mission systems identification for the upgrade design analysis of anti-submarine maritime helicopters-an update 31st European Rotorcraft Forum. 2005. |
0.303 |
|
| 2004 |
Johnson EN, Schrage DP. System integration and operation of a research unmanned aerial vehicle Journal of Aerospace Computing, Information and Communication. 5-18. DOI: 10.2514/1.4424 |
0.382 |
|
| 2004 |
Jonnalagadda S, Sinha AK, Hoffmann P, Schrage DP. Modelling upgrade design of maritime helicopters for anti-submarine missions - Project framework Annual Forum Proceedings - American Helicopter Society. 1: 1120-1128. |
0.388 |
|
| 2004 |
Mavris DN, Collins KB, Schrage DP. A method of qualitative analysis during conceptual design as applied to unmanned aerial vehicles Annual Forum Proceedings - American Helicopter Society. 1: 642-655. |
0.344 |
|
| 2003 |
DeLaurentis DA, Lewe JH, Schrage DP. Abstraction and modeling hypothesis for future transportation architectures Aiaa\Icas International Air and Space Symposium and Exposition: the Next 100 Years. |
0.756 |
|
| 2003 |
Lewe JH, Upton EG, Mavris DN, Schrage DP. An agent-based framework for evaluating future transportation architectures Aiaa's 3rd Annual Aviation Technology, Integration, and Operations (Atio) Forum. |
0.698 |
|
| 2002 |
Lewe JH, Ahn BH, Delaurentis DA, Mavris DN, Schrage DP. An integrated decision-making method to identify design requirements through agent-based simulation for personal air vehicle system Aiaa's Aircraft Technology, Integration, and Operations (Atio) 2002 Technical Forum. |
0.791 |
|
| 2001 |
Wills L, Kannan S, Sander S, Guler M, Heck B, Prasad JVR, Schrage D, Vachtsevanos G. An open platform for reconfigurable control Ieee Control Systems Magazine. 21: 49-64. DOI: 10.1109/37.924797 |
0.675 |
|
| 2001 |
Baker AP, Mavris DN, Schrage DP. The role of requirements in conceptual aircraft design and their interactions with technologies and vehicle attributes 1st Aiaa, Aircraft, Technology Integration, and Operations Forum. |
0.417 |
|
| 2000 |
Zink PS, DeLaurentis DA, Hale MA, Volovoi VV, Schrage DP, Craig JI, Fulton RE, Mistree F, Mavris DN, Chen W, Lewis KE, Cesnik CES, Röhl PJ, Koch PN, Simpson TW. New approaches to high speed civil transport multidisciplinary design and optimization Ieee Aerospace Conference Proceedings. 1: 355-369. |
0.547 |
|
| 2000 |
Hale MA, Daberkow DD, DeLaurentis DA, Mavris DN, Schrage DP, Craig JI. Capturing Corporate Philosophy: The Future of IT Proceedings of the Joint Conference On Information Sciences. 5: 667-670. |
0.475 |
|
| 1999 |
Laps T, Burdun IY, Mavris DN, Schrage DP. Method for the exploration of cause and effect links and derivation of causal trees from accident reports Sae Technical Papers. DOI: 10.4271/1999-01-1433 |
0.366 |
|
| 1998 |
Marx WJ, Mavris DN, Schrage DP. Cost/Time Analysis for Theoretical Aircraft Production Journal of Aircraft. 35: 637-646. DOI: 10.2514/2.2348 |
0.378 |
|
| 1998 |
Marx WJ, Mavris DN, Schrage DP. A knowledge-based system integrated with numerical analysis tools for aircraft life-cycle design Artificial Intelligence For Engineering Design, Analysis and Manufacturing: Aiedam. 12: 211-229. DOI: 10.1017/S0890060498123016 |
0.482 |
|
| 1997 |
Tai JC, Mavris DN, Schrage DP. A comparative assessment of high speed rotorcraft concepts (HSRC): Reaction driven stopped rotor/wing versus variable diameter Tiltrotor Sae Technical Papers. DOI: 10.4271/975548 |
0.454 |
|
| 1997 |
Tapia F, Sankar LN, Schrage DP. An inverse aerodynamic design method for rotor blades Journal of the American Helicopter Society. 42: 321-326. DOI: 10.4050/Jahs.42.321 |
0.483 |
|
| 1997 |
Tai JC, Mavris DN, Schrage DP. A comparative assessment of highspeed rotorcraft concepts (HSRC): Reaction driven stopped rotor/wing and variable diameter tiltrotor World Aviation Congress, 1997. DOI: 10.2514/6.1997-5548 |
0.343 |
|
| 1997 |
Chen W, Allen JK, Schrage DP, Mistree F. Statistical experimentation methods for achieving affordable concurrent systems design Aiaa Journal. 35: 893-900. DOI: 10.2514/2.7464 |
0.463 |
|
| 1997 |
Mavris DN, Bandte O, Schrage DP. Effect of Mission Requirements on the Economic Robustness of an HSCT Concept Journal of Parametrics. 17: 53-77. DOI: 10.1080/10157891.1997.10462558 |
0.75 |
|
| 1997 |
Mavris DN, Baker AP, Schrage DP. IPPD through robust design simulation for an affordable Short Haul Civil Tiltrotor Annual Forum Proceedings - American Helicopter Society. 2: 1615-1625. |
0.41 |
|
| 1997 |
DeLaurentis DA, Mavris DN, Calise AJ, Schrage DP. Generating dynamic models including uncertainty for use in aircraft conceptual design 22nd Atmospheric Flight Mechanics Conference. 367-376. |
0.366 |
|
| 1996 |
Tai JC, Mavris DN, Schrage DP. An assessment of a reaction driven stopped rotor/wing using circulation control in forward flight Sae Technical Papers. DOI: 10.4271/965612 |
0.462 |
|
| 1996 |
Delaurentis D, Zink PS, Mavris D, Cesnik CES, Schrage DP. New approaches to multidisciplinary synthesis: An aero-structures-control application using statistical techniques Sae Technical Papers. DOI: 10.4271/965501 |
0.64 |
|
| 1996 |
Stettner M, Mavris DN, Schrage DP. A method for flexible design integration 37th Aiaa/Asme/Asce/Ahs/Asc Structure, Structural Dynamics and Materials Conference. 1899-1907. DOI: 10.2514/6.1996-1540 |
0.371 |
|
| 1996 |
Marx WJ, Mavris DN, Schrage DP. Effects of alternative wing structural concepts on high speed civil transport life cycle costs 37th Aiaa/Asme/Asce/Ahs/Asc Structure, Structural Dynamics and Materials Conference. 562-582. DOI: 10.2514/6.1996-1381 |
0.387 |
|
| 1996 |
Hale MA, Craig JI, Mistree F, Schrage DP. DREAMS and IMAGE: A model and computer implementation for concurrent, life-cycle design of complex systems Concurrent Engineering Research and Applications. 4: 171-185. DOI: 10.1177/1063293X9600400207 |
0.504 |
|
| 1996 |
Delaurentis DA, Carlos CE, Lee JM, Mavris DN, Schrage DP. A new approach to integrated wing design in conceptual synthesis and optimization 6th Symposium On Multidisciplinary Analysis and Optimization. 1835-1843. |
0.391 |
|
| 1996 |
Mavris DN, Bandtev O, Schrage DP. Application of probabilistic methods for the determination of an economically robust hsct configuration 6th Symposium On Multidisciplinary Analysis and Optimization. 968-978. |
0.323 |
|
| 1996 |
Chen W, Schrage DP, Alien JK, Mistree F. Statistical experimentation for affordable concurrent design 6th Symposium On Multidisciplinary Analysis and Optimization. 921-930. |
0.395 |
|
| 1995 |
Hale MA, Craig JI, Mistree F, Schrage DP. On the development of a computing infrastructure that facilitates IPPD from a decision-based perspective Aircraft Engineering, Technology, and Operations Congress. |
0.317 |
|
| 1995 |
Schrage DP, Mavris DN. Integrated product/process design/development (IPPD) through robust design simulation: The key for affordable systems Aircraft Engineering, Technology, and Operations Congress. |
0.433 |
|
| 1995 |
Tai JC, Mavris DN, Schrage DP. Application of a response surface method to the design of tip jet driven stopped rotor/wing concepts Aircraft Engineering, Technology, and Operations Congress. |
0.402 |
|
| 1992 |
Calise AJ, Wasikowski ME, Schrage DP. Optimal output feedback for linear time-periodic systems Journal of Guidance, Control, and Dynamics. 15: 416-423. DOI: 10.2514/3.20852 |
0.382 |
|
| 1989 |
Schrage D, Costello M, Mittleider D. Design Concepts for an Advanced Cargo Rotorcraft Journal of the American Helicopter Society. 34: 56-65. DOI: 10.4050/Jahs.34.56 |
0.456 |
|
| 1986 |
Schrage DP. Use of rotorcraft computer analysis for U.S. government design assessment Computers and Mathematics With Applications. 12: 1-9. DOI: 10.1016/0898-1221(86)90085-4 |
0.344 |
|
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