Airframe development for the Hybrid Wing Body aircraft

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Velicki, Alex ^a   Thrash, Patrick ^a   Jegley, Dawn ^b  

^a BOEING COMPANY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFRAMES; CABINS (AIRCRAFT); FUSELAGES; LIFT DRAG RATIO; NASA; STRUCTURAL FRAMES;

AIRFRAME STRUCTURES; AIRPLANE PERFORMANCE; HIGHER-ORDER; LIFT TO DRAG RATIO; WEIGHT SAVING; WING BODY AIRCRAFT;

WINGS;

EID: 78549231995     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-932     Document Type: Conference Paper

References (9)

1. Liebeck, R. H., "DESIGN OF THE BLENDED-WING-BODY SUBSONIC TRANSPORT", 2002 Wright Brothers Lecture, AIAA Paper 2002-0002, August 2002.
2. Velicki, A. and Thrash, P.J., "Blended Wing Body Structural Concept Development", Royal Aeronautical Society Aircraft Structural Design Conference Challenges for the Next Generation - Concept to Disposal, 14-16 October 2008, Liverpool, UK.
3. AIR VEHICLE TECHNOLOGY INTEGRATION PROGRAM (AVTIP), Delivery Order 0059: Multi-role Bomber Structural Analysis, AFRL-VA-WP-TR-2006-3067, Krishna Hoffman, MAY 2006, Final Report for 14 December 2004 - 08 May 2006, AFRL-VA-WP-TR-2006- 3067.
4. Velicki, A. and Thrash, P.J., "Damage Arresting Composites for Shaped Vehicles", NASA Contract NNL07AA48C, Phase I Final Report for October 2007 through September 2008, released November 2008.
5. Hinrichs, S., "General Methods for Determining Stitched Composite Material Stiffnesses and Allowable Strengths, Vol I," McDonnell Douglas Technical Report MDC94K9113, Long Beach CA, March 1995.
6. Warp/knit Multi-Axial Carbon Fiber Fabric, The Boeing Company, Process Specification DMS 2436H, Long Beach CA, 2005.
7. Velicki, A. and Thrash, P.J., "Advanced Structural Concept Development Using Stitched Composites", 49th AIAA/ASME/ASCE/SHS/ASC Structures, Structural Dynamics, and Materials Conference, 7-10 April 2008, Schaumburg, IL, AIAA Paper 2008-2329.
8. Jegley, D.C., Velicki, A., Hansen, D., "Structural Efficiency Of Stitched Rod-stiffened Composite Panels With Stiffener Crippling", 49th AIAA/ASME/ASCE/SHS/ASC Structures, Structural Dynamics, and Materials Conference, 7-10 April 2008, Schaumburg, IL.
9. Ambur, D. A., Rouse, M., Starnes, J.H., and Shuart, M. J., "Facilities for Combined Loads Testing of Aircraft Structures to Satisfy Structural Technology Development Requirements. Presented at the 5th Annual Advanced Composites Technology Conference, Seattle, WA, August 22-36, 1994.