Advanced Shipboard Landing Aerodynamic Interference Software Modules

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$743,034.00
Award Year:
2002
Program:
SBIR
Phase:
Phase II
Contract:
N68335-02-C-0018
Agency Tracking Number:
N011-0135
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Advanced Rotorcraft Technology, Inc.
1685 Plymouth Street Suite 250, Mountain View, CA, 94043
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
149732315
Principal Investigator:
Chengjian He
Director of IR&D
(650) 968-1464
he@flightlab.com
Business Contact:
Ronald DuVal
President
(650) 968-1464
ron@flightlab.com
Research Institution:
n/a
Abstract
"This SBIR is intended to develop a high fidelity modeling andsimulation tool to support shipboard rotorcraft operationanalysis. The efforts address not only the enhancement of eachindividual modeling discipline that is related to the simulationof rotorcraft shipboard testing, but also their integration intoa comprehensive simulation environment to allow forrotorcraft/ship interaction. The proposed development willresult in a rotorcraft shipboard operational envelope evaluationtool that can be applied to facilitate the test and evaluationprocess to enhance flight test productivity, reduce cost, andincrease the safety of flight test operations. The proposal emphasizes the high fidelity modeling andsimulation of the aerodynamic and dynamic interaction betweenrotorcraft and ship. The innovations of this proposal aresummarized as: (1) Development of a modeling and simulation tool to supportrotorcraft shipboard operation. This includes advanced modelingof the aerodynamic interference of the rotor wake, the shipairwake, the ship turbulence, and their interaction. It alsoincludes accurate evaluation of the rotorcraft shipboard dynamicinterface testing envelope to effectively support the rotorcraftshipboard test and evaluation process. (2) Development of a comprehensive simulation tool forrotorcraft shipboard operation analysis. This includes modelingand simulation/analysis of the rotorcraft engagement anddisengagement operation, rotorcr

* information listed above is at the time of submission.

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