Aeronautical Engineering Projects
Analysis of the effects of a refueling system on the KC-135R for AEL Industries (now BAE Systems).
Computer aided drafting work on a twin-engine propeller all-composite experimental airplane for DreamWings. Design includes stability and control analysis for one airplane with three different engines.
Stability and control derivatives for the Cessna Citation II for Alpha Systems, a simulator company.
Preliminary design and analysis on the Kelly Space and Technology Second Generation Reusable Launch Vehicle under the NASA NRA8-27 contract.
Design and analysis for Freewing.
Weight and moment of inertia prediction of the Cessna Caravan for Kohlman Systems Research.
Design verification, aerodynamic, stability and control support for a small business jet for Safire Aircraft.
Aerodynamic model and weight/moments of inertia of the Piper Malibu Mirage for SimCom.
Design of a new series of experimental and LSA class airplanes for TranscendX Corp.
Design and CAD work for Milner Aircar.
Two-seat, experimental category carbon fiber kit airplane.
Part of the control system for a two-seat, experimental category carbon fiber kit airplane.
Mechanical and interior systems layout for a two seat kit airplane
Carbon fiber wings for two-seat experimental category airplane under construction
A wing plug being milled to make a mold for a two place experimental airplane.
Complete loads analysis and control system design of a two-seat all composite ultralight/experimental airplane for DreamWings, LLC.
Water tunnel tests on a modified KC-135R for AEL Industries (now BAE Systems).
Load testing of the carbon fiber wing of a two-seat experimental category kit airplane.
Impact Resistance Testing and evaluation of various composite panel skin materials.
First flight of a new LSA category composite airplane, the Nexaer LS-1, on October 16, 2006. DARcorporation was involved with design and development.
First flight of Experimental category, two seat, carbon fiber airplane for DreamWings, LLC.
Landing, first flight of Experimental, two-place carbon fiber kit airplane designed, built and tested under guidance of DARcorporation.
Design & Modification
- Verification of a new design of a 6 passenger propeller airplane. Analysis included vertical tail sizing and wing sizing
- Investigation of forward maneuver area air-delivery systems for the US Navy, US Marine Corps. Creation of a simulation program for air dropping payload. Preliminary design of new airplanes to be used for delivering payload in war-zones
- Design verification of several fire-fighting airplanes for Air Tractor. Preliminary design verification and performance analysis on a family of small airplanes
- Design verification of a single engine airplane for Air Tractor. Design verification and performance analysis on a family of small airplanes. Analysis of competitor airplanes and comparison with new designs. Stability and control verification, including control forces
- New design of a two person kit airplane. Preliminary design of two airplanes based on an existing kit airplane
- NASA SBIR Phase II contract: development of G.A.-CAD: General Aviation Computer Aided Design. To revitalize the General Aviation industry, NASA Langley awarded DARcorporation a contract to design a preliminary design and analysis tool for PC’s including structural design and drafting capability
- Preliminary Design of a small freighter/passenger airplane for NEXUS
- New design of an all composite two person kit airplane for DreamWings. Design includes stability and control analysis for one airplane with three different engines
- Design verification of a twin engine airplane for Air Tractor. Analysis of competitor airplanes and comparison with new designs. Stability and control verification, including control forces
- Design verification and stability and control analysis on the VisionAire Vantage business jet
- Complete loads analysis and control system design of a two-seat all composite ultralight/experimental airplane for DreamWings
- Design studies for Air Tractor on single-, twin- and three-engine airplanes
- Preliminary design of a two-seat single engine jet-trainer
- Preliminary design of a family of 4-6 seat twin-engine jets
- Preliminary sizing of a small business twin-engine jet for Safire
- Control system design for the DeamWings Valkyrie
- Preliminary design and analysis on the Kelly Space and Technology Second Generation Reusable Launch Vehicle under the NASA NRA8-27 contract
- Design verification, aerodynamic, stability and control support for a small business jet for Safire Aircraft
- Preliminary design of a supersonic business jet for OrthoAir
- Preliminary design of a 4-seat business jet
- Conceptual design of a single engine 4-seat G.A. airplane
- Preliminary design of a personal air vehicle capable of vertical take-off
- Preliminary design of a twin engine 6-seat G.A. airplane
- Firewall forward design of an ATP turboprop powered Vans RV-6A for Rivers Aeronautical
- Design verification of a UAV concept.
- Preliminary design of a jet powered UAV concept
- Preliminary design of a Sport Pilot class airplane for Composicraft
- Preliminary design verification of a 4-seat G.A. airplane
- Speedbrake design for a small business jet
- Preliminary design of a transonic business jet
- Preliminary design of a roadable aircraft for Aerocar
- Control system design for a VTOL UAV
- Propeller/Rotor design for Freewing Flight Technologies, Inc.
- Preliminary design of the Milner AirCar
- Design evaluation of the Hensley Wolf twin propeller pusher 4-seater
- Preliminary design of a 4-seat G.A. Airplane
- Design review for the Nexaer LS1
- Preliminary design of a twin pusher G.A. airplane
- Design review for D-Star Engineering
- Design review for Finite Engineering
- Design review for Trolltune Corporation
- Design of a VTOL UAV for Freewing
- Design review on a UAV
- Design review for an LSA
- Design of a scaled Supermarine Spitfire
- Structural design of the Valkyrie composite experimental airplane for DreamWings
- The University of Kansas/NASA DC-8 Antenna Assembly Aerodynamic and Structural Design and Analysis
- Samson Motorworks: Switchblade preliminary design analysis
- Samson Motorworks: Switchblade wing mechanism design
- Liaoning Ante Steel Structure Group vertical wind tunnel aerodynamic and structural design and analysis
- University of Kansas/NASA P-3B antenna assembly design, simulation (aerodynamic and structural analyses)
- Modification of the horizontal tail of a commuter aircraft for Fairchild Aircraft
- Analysis of stick forces, longitudinal stability and control and verification with airworthiness standards. Analysis included ground effects, flap effects and propeller slipstream effects
- Analysis of the stability and control including stick forces and gradients for a KC-135R with a fuselage mounted external refueling system
- Stability and control derivatives for the Beech Bonanza for a MDM Systems, Inc. a simulator company. All stability and control derivatives are determined for several flight conditions to create a flight simulator model
- Stability and lift analysis of a 6-seater General Aviation aircraft for Hutterer Engineering
- Stability and control derivatives for the Cessna Citation II for Alpha Systems, a simulator company. All stability and control derivatives are determined for several flight conditions to create a flight simulator model
- Air Tractor stability and control analysis
- Analysis of the effects of a refueling system on the KC-135R for AEL Industries (now BAE Systems)
- Analysis of flow effects on the horizontal tail for a modified KC-135R with a fuselage mounted external refueling system
- Analysis of flow fields under the fuselage of a Boeing 707 for locating the best position of a refueling system
- Derivation of a system of equations of motion for Precision Training Software, a simulator company. Mathematical equations are derived for a training simulator
- Weight and moment of inertia prediction of the Cessna Caravan for Kohlman Systems Research
- Horizontal tail analysis for a 2-seat amphibious airplane
- Loads analysis for the Snow S-22
- Equations of motion for the tilt-boom concept for Freewing Flight Technologies, Inc.
- UAV database development for Thomas International
- Patent support work for a VTOL concept
- Competitor analysis for a small business jet manufacturer
- Initial structural analysis for Milner AirCar
- Simulation model of an Air Tractor 502B for SimCom
- CAD drawings of the wing ribs of the WWII Mitsubishi Zero
- CAD for a roadable aircraft concept
- CAD drawings for the horizontal tail of the WWII Mitsubishi Zero
- CFD analysis of a small business jet
- CFD analysis for Milner AirCar
- CFD analysis of a bird deflector system for jet engines
Manufacturing & Testing
- Samson Motorworks: Display Mockup Construction
- Development of techniques to interface CAD with CAM to manufacture plugs and molds for DreamWings
- Computer aided drafting work on a twin-engine propeller all-composite experimental airplane for DreamWings
- Wind tunnel test for Safire Aircraft Company
- Wind tunnel test management for Safire Aircraft
- Design and wind tunnel testing of a wind measuring device
- Wind tunnel test program management for a small business jet
- Aerodynamic design and wind tunnel testing of a flying toy
- Wind Tunnel data analysis for a small business jet
- Wind Tunnel program management for Piper Aircraft Corporation on the PiperJet
- Windtunnel tests and project management for a small business jet for VisionAire Corporation
- Water tunnel tests on a modified KC-135R for AEL Industries (now BAE Systems)
- Water tunnel tests on a Boeing 707-320B for AEL Industries (now BAE Systems)
- Water tunnel tests on a small business jet for VisionAire Corporation
- Ground test development and test management for a propeller propulsion system
- VTOL Propulsion ground test
- Test support for a VTOL UAV
- Load tests of NASA P-3B Orion wing with antenna fairing installations and modal tests of antenna fairing installations on NASA P-3B Orion wing to obtain natural frequencies and mode shapes
- Manufacturing of Antenna fairing pylons for NASA P-3B Orion and installation of NASA P-3B Orion antenna fairings
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