NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- A1.06-2083
SUBTOPIC TITLE:
 Vertical Lift Technology and Urban Air Mobility
PROPOSAL TITLE:
 Comprehensive Acoustic Analysis for Distributed Electric Propulsion Aircraft
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Continuum Dynamics, Inc.
34 Lexington Avenue
Ewing , NJ 08618-2302
(609) 538-0444

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Mr. Daniel Wachspress
dan@continuum-dynamics.com
34 Lexington Avenue Ewing, NJ 08618 - 2302
(609) 538-0444

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Ms. Barbara Agans
barbara@continuum-dynamics.com
34 Lexington Avenue Ewing, NJ 08618 - 2302
(609) 538-0444
Estimated Technology Readiness Level (TRL) :
Begin: 3
End: 4
Technical Abstract

A major innovative thrust in urban air mobility (UAM) is underway that will potentially transform how we travel by providing on-demand, affordable, quiet, and fast passenger-carrying operations in metropolitan areas.  As cited in the NASA SBIR A1.06 topic solicitation, “Growth of UAM is dependent on affordable, low-noise VTOL configurations, which may be enabled by electric aircraft propulsion technologies.”  To support this, NASA implemented the DELIVER (Design Environment for Novel Vertical Lift Vehicles) program to help “… bring 100 years of aeronautics knowledge to the new entrepreneur’s desktop with a design environment for emerging vertical lift vehicles.”  DELIVER identified a key gap in technology required by UAM vehicle developers – “no current ability to account for noise in conceptual design”.  The proposed effort is directed toward filling this technology gap by enhancing state-of-the-art rotary-wing aeroacoustics analysis with the key additional modeling capabilities needed for comprehensive acoustic prediction of Distributed Electric Propulsion (DEP) aircraft noise.  The new tool will provide fast, accurate prediction of all the acoustic characteristics associated with DEP aircraft, including (1) noise generated by the simultaneous operation of multiple, variable RPM lifting and propelling rotors and props, (including stacked and counter-rotating blades), (2) interacting propeller/duct/airframe noise, (including strut noise and prop/wing interaction noise), (3) full-spectrum broadband noise modeling pertinent to this new class of aircraft, and (4) electric motor noise.  The new software will also include auralization capabilities to enhance evaluation of community annoyance due to various acoustics characteristics beyond A-weighted sound pressure level.

Potential NASA Applications

The proposed effort directly supports NASA’s ARMD’s SIP strategic thrusts 3 (ultra-efficient sub/transonic aircraft) and 3B (NASA Vertical Lift Strategic Direction) by enabling accurate prediction and optimization of DEP aircraft noise characteristics and sources during the conceptual design phase.  As identified by NASA, the lack of this capability is a critical gap impeding the progress of current UAM vehicle development. 

Potential Non-NASA Applications

CDI collaborates with many UAM vehicle developers who have an immediate need for the proposed analysis capability to predict DEP aircraft noise in the conceptual design phase.  Commercialization to these customers would be concurrent with the SBIR effort.  The analysis will also be of great value to the DoD and major rotorcraft manufacturers in analyzing acoustic characteristics of future compound aircraft, like the SB>1 Defiant, V-280 Valor, AVX CCH, and Aurora Lightning Strike.


Form Generated on 05/25/2018 11:27:07