SBIR-STTR Award

Maneuvering Rotorcraft Aeromechanics
Award last edited on: 5/16/2003

Sponsored Program
SBIR
Awarding Agency
NASA : ARC
Total Award Amount
$670,000
Award Phase
2
Solicitation Topic Code
-----

Principal Investigator
Brooke C Smith

Company Information

AeroArts LLC

PO Box 2909
Palos Verdes Peninsu, CA 90274
   (310) 548-0927
   info@AeroArts.com
   www.AeroArts.com
Location: Single
Congr. District: 33
County: Los Angeles

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2002
Phase I Amount
$70,000
Rotary-wing vehicles proposed for improved system capacity must meet civil global aviation requirements for safety, efficiency, and affordability. To achieve the needed advances, greatly improved modeling is required. Many advances have been made in measuring dynamic characteristics of rotary-wing vehicles, for example by Tischler et al. However, innovative advances are needed in methods to capture the dynamic and cross-coupling effects that are still a challenge and impediment to rapid design cycles. A very recent advance in test techniques utilizes water as a test medium for dynamic testing. This method circumvents many of the problems presented by air as a medium, by allowing testing in slow motion, by separating model and test support frequencies, by greatly improving signal-to-noise ratios, and by allowing the traditional advantages of the familiar water tunnel or channel, with its unparalleled flow visualization. POTENTIAL COMMERCIAL APPLICATIONS The ability to predict maneuvering aerodynamics and stability parameters early in the development cycle will reduce the time, risk, and cost of new rotorcraft. The methods described herein also apply to high performance aircraft development

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2003
Phase II Amount
$600,000
___(NOTE: Note: no official Abstract exists of this Phase II projects. Abstract is modified by idi from relevant Phase I data. The specific Phase II work statement and objectives may differ)___ Rotary-wing vehicles proposed for improved system capacity must meet civil global aviation requirements for safety, efficiency, and affordability. To achieve the needed advances, greatly improved modeling is required. Many advances have been made in measuring dynamic characteristics of rotary-wing vehicles, for example by Tischler et al. However, innovative advances are needed in methods to capture the dynamic and cross-coupling effects that are still a challenge and impediment to rapid design cycles. A very recent advance in test techniques utilizes water as a test medium for dynamic testing. This method circumvents many of the problems presented by air as a medium, by allowing testing in slow motion, by separating model and test support frequencies, by greatly improving signal-to-noise ratios, and by allowing the traditional advantages of the familiar water tunnel or channel, with its unparalleled flow visualization. POTENTIAL COMMERCIAL APPLICATIONS The ability to predict maneuvering aerodynamics and stability parameters early in the development cycle will reduce the time, risk, and cost of new rotorcraft. The methods described herein also apply to high performance aircraft development