John Cipolla's Resume Page

Philosophy
"Never make someone a priority in your life when you are just an option in theirs"
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WHY Consider John Cipolla and AeroRocket
Demonstrated exceptional creativity in Computational Fluid Dynamics (CFD), Finite Element Analysis (FEA) and composite material analysis for aerospace applications. Proven computer programming ability using Microsoft Visual Basic, FORTRAN and C++. Not just theoretical but "real world" experience in subsonic, supersonic and hypersonic wind tunnel testing and related CFD analysis and experiments. Highly experienced in the industrial use of sophisticated numerical analysis techniques to enhance productivity and reduce final product cost.

John Cipolla
Chief Aerodynamicist
AeroRocket and WarpMetrics

Professional Interests
Aerodynamics, structures, materials, applied mechanics and space propulsion.
Also, Computational Fluid Dynamics (CFD), wind tunnel testing, Finite Element Analysis (FEA), General Relativity, quantum mechanics, particle physics and composite materials analysis & design.

Wind Tunnel Testing and Aerodynamics
AeroRocket provides wind tunnel testing for the determination of LIFT (CL) and DRAG (CD) coefficients for almost any aerodynamic shape using its own subsonic wind tunnel for the low cost of only $25 per hour. The wind tunnel at AeroRocket's disposal was developed in-house to provide a wide range of lift, drag, velocity and pressure profile measurements for any shape imaginable. The test section is 7 inches wide x 10 inches high x 16 inches long. Maximum test section velocity is 80 ft/sec without a test item installed. The AeroRocket wind tunnel is ideal for measuring the subsonic drag of unusual designs and shapes not treated by AeroDRAG™ or other rocket analysis computer programs until the development of AeroCFD® and VisualCFD™. The AeroRocket subsonic wind tunnel is ideal for measuring drag and lift using the in-house built two-component force balance system. The AeroRocket subsonic wind tunnel is routinely used for defining the aerodynamic properties of new designs and for validating the design of vehicles like the Schafer Corporation ultra-high altitude V-Ship.

AeroRocket's new supersonic blow-down wind tunnel having an inside-diameter of 1.03 inches and Mach 3 capability is operational and being used to design the HFV-3X spacecraft for transonic and supersonic flow. In addition, John Cipolla's unique expertise in the fabrication of miniature supersonic wind tunnel models allows testing realistic shapes for accurate flow field and CD measurements for a wide variety of R&D applications, including the HFV-3X and other supersonic designs.
                                           
Primary Aerospace/Mechanical engineer for the 800 foot long Aeroballistic Research Facility (ARF) located at Eglin AFB in Florida. For ARF development, John Cipolla designed the free-flight instrumentation used to measure subsonic, supersonic and hypersonic projectile position, velocity, stability derivatives (CNa, CMa) and aerodynamic coefficients (Xcp, Cd, CL). Free-flight tests conducted in the ARF are used to validate innovative high speed projectile designs and related Computational Fluid Dynamics results. The ARF engineering design effort continues to have a direct positive impact on many Army, USAF and NASA projects. John Cipolla utilized the ARF to publish papers concerning the Interferometric analysis of a cone-cylinder-flare body in hypersonic flight and the analysis of slender missile configurations in supersonic flight.


Computational Fluid Dynamics (CFD) and Propulsion
CFD EXPERIENCE: Project manager and principal developer of new Computational Fluid Dynamics and rocket analysis computer software. Developed AeroCFD® for the subsonic analysis of model rockets and VisualCFD™ for the compressible fluid flow analysis of full-scale rockets. VisualCFD™ is a three-dimensional axisymmetric and two-dimensional finite-volume numerical analysis computer program that solves the steady and unsteady inviscid Euler equations for subsonic, transonic, and supersonic flow. VisualCFD™ generates flow fields by applying automatic numerical grid generation and mesh distribution around a library of standard aerodynamic shapes. Complex CFD solutions are achieved in minutes rather than hours greatly increasing aerodynamic design productivity.

PROPULSION EXPERIENCE: Developed AeroIsp™ an affordable program for the generation of  thrust-time predictions for new solid fuel rocket motors and curve-fit analyses of new rocket propellants. Developed several other software applications for the analysis of model rocket, high power rocket and professional (full-scale) rocket aerodynamics. Specifically, developed Nozzle and AeroSpike for the performance analysis of standard nozzles and the next generation aerospike rocket motors. For the Strategic Defense Initiative (SDI) developed the first magnetic field finite element analysis (FEA) computer program for determining the internal and external forces experienced by electro-magnetically (EM) propelled hypervelocity projectiles. Later, other companies developed similar magnetic field finite element analysis capability, but John Cipolla's magnetic field finite element analysis was the first available at Eglin AFB for modeling electro-magnetically launched hypervelocity projectiles.

FLUENT and GAMBIT used to solve complex 3-dimensional turbulent fluid flows in process control valves. Using Fluent CFD John Cipolla invented an innovative valve trim or insert capable of controlling cavitation and reducing valve induced noise level by several dB. This new valve insert design was made possible because John Cipolla was able to draw upon previous aerospace experience where similar methods and devices are used to reduce sound pressure level in aircraft open bomb bays when operating in the transonic, supersonic and hypersonic environment.

Related Aerodynamics and CFD Experience
--Software development for new grid generation and CFD flow solver algorithms.
--Project manager for a USAF project to analyze separation of bodies in hypersonic flow.
--Developed methods to model high-temperature equilibrium flows for hypersonic vehicles.
--Program management of new CFD program code development at Wright Laboratory.
--Aeroelastic and structural analyses of F-15, F-16, A-10 and B-52 aircraft/weapon compatibility.
--Participated in the development of electro-magnetically (EM) launched projectiles for SDI.
--Aerodynamics and structural analyses for the AMRAAM air-to-air missile.

John Cipolla's "firsts" in the areas of aerodynamics and CFD
--Developed 3-D multi-block missile CFD model using the CRAY-2 super computer.
--Developed a fully viscous cavity flow CFD simulation of a fighter aircraft open bomb bay.
--Predicted total missile drag and free flight static stability derivatives using EAGLE CFD code.

Aerospace Structural Analysis
Experienced in the industrial use of sophisticated Finite Element Analysis (FEA) methods to enhance productivity and reduce final product cost. This valuable experience has been in the areas of static and dynamic analyses using MSC/NASTRAN and COSMOS/M finite element analysis software. Developed and coded several FEA computer programs for USAF in-house use in the areas of structural analysis, fluid dynamics and electromagnetic and magnetic fields. Experience using AutoCAD and ProEngineer computer aided design software for sophisticated design efforts. Finally, solid experience using PDEase2D for the analysis of field problems in structural mechanics and fluid dynamics.

STRUCTURAL ANALYSIS: Performed complex structural and aeroelastic analyses of USAF aircraft/store compatibility for flight test certification. Planed and performed engineering studies for the design and flight test of weapons being procured by the Air Force Materiel Command. Incorporated several new armament and launcher combinations into the F-15 and F-16 aircraft flutter simulations. This work required in-depth knowledge of MSC/NASTRAN to perform aeroelastic and flutter simulations of the F-111, F-15 and F-16 aircraft. During Desert Storm, certified the GBU-28 laser guided super bomb called the "Bunker Buster" for carriage aboard the F-111 and F-15 aircraft. Finally, for the Strategic Defense Initiative (SDI) analyzed the dynamic response of EM launched kinetic kill vehicles (KKV) accelerated to 100,000 G's. MSC/NASTRAN and classical stress analyses used to determine Von Mises stress levels in the projectile airframe during electro-magnetic rail gun launch.

COMPOSITE MATERIALS: While working for the USAF developed the algorithm and matrix equation solution for the in-house paper, "Aeroelastic Analysis of a Forward-Swept Wing with Stiffness Cross-Coupling". This analysis made possible the rapid parametric design of composite material forward-swept wings. Also, experienced in the theoretical analysis of aerospace structures that use composite materials for stiffness cross-coupling like forward-swept wings, composite shells and single-piece filament-wound graphite epoxy casings for solid fuel rocket motors. Developed methods to model carbon-carbon composite material nose cone ablation for EM launched SDI projectiles. Also, performed a finite element structural analysis for an early GBU-15 composite-wing transonic de-lamination problem.

PIEZOELECTRIC MATERIALS (ACOUSTICS): While working for Raytheon developed a FORTRAN-77 based computer program for the design of underwater sonar transducers. PESAP (Piezo-Electric Structural Analysis Program) incorporated an electrodynamic piezoelectric finite element in addition to the standard constant strain finite element. PESAP successfully predicted resonance frequency, modal patterns, input electrical admittance verses frequency and modal displacements for several U.S. Navy underwater sonar transducers. PESAP more accurately modeled the interaction between complex modes of vibration and the acoustic environment than other methods that were available.

Warp Drive Basic Research
John Cipolla is performing innovative new research in the area of warp drive technology for faster than light star travel. The image to the left shows a spacecraft being propelled while enclosed within an artificially generated warp bubble.

A warp bubble based on the concepts of General Relativity uses opposing regions of expanding and contracting spacetime for propelling a starship at velocities exceeding the speed of light. This is a work in progress based on a new method for warping spacetime to generate warp bubble disturbances without the need for exotic matter or negative energy.

Computer Programming Experience
Self-employed aerospace engineer and computer programmer. Deeply involved in desktop publishing for the Internet and the application of computer programs for producing high impact graphics and animations for e-commerce web pages. Extensive experience using UNIX, Microsoft Windows and Macintosh operating systems.

Related Computer Programming Experience
--CFD code development using FORTRAN-77.
--Developed AeroDRAG™ to compute rocket drag to Mach 20.
--Developed CFD applications for model rockets: AeroCFD® & 2D-WING™, etc.
--Developed CFD applications for high speed rockets: HyperCFD™ and VisualCFD™.
--Experienced in industrial R&D and web page computer programming.
--Create, operate and manage the AeroRocket e-Commerce web site.
--Internet publishing using Microsoft FrontPage, Adobe Photoshop, Adobe Illustrator.
--Automated several ASME Code pressure vessel design computer programs using VB-6.
--Mathematical capability enhanced by Maple V, MathCAD, Theorist and Excel.

Patents and Trademarks
John Cipolla registered the AeroCFD® trademark (number 2992220) with the United Stares Patent and Trademark Office on September 6, 2005 for the following description of Goods and Services: COMPUTER SOFTWARE THAT USES THE METHODS OF COMPUTATIONAL FLUID DYNAMICS (CFD) FOR THE PREDICTION OF MODEL ROCKET DRAG, LIFT AND MOMENT COEFFICIENTS; THIS SOFTWARE IS USED FOR DESIGNING MORE AERODYNAMICALLY EFFICIENT ROCKETS.

Some Technical Publications
1. V-Ship Wind Tunnel Drag and Lift Estimation Compared to Cylinder Cross-Flow Simulation. Schafer Corp.
2. Spool Rocket Drag and Center of Pressure Measurement. Developed using the AeroRocket wind tunnel.
3. Fluent Multi-Phase Control Valve Analysis; Process Control Valve Cavitation and Noise Analysis. New design patent.
4. Elastic-Plastic Finite Element Analysis (FEA) of an Elliptical Pipe for High Pressure/Temperature Application.
5. Computational and Experimental Interferometric Analysis of a Cone-Cylinder Flare Body; AIAA paper.
6. Aerodynamic Test and Analysis of a Slender Generic Missile Configuration; AIAA paper.
7. Program EAGLE Users Manual, Introduction and Grid Applications; AFATL-TR-88-117, Vol. I and Vol. II.
8. Radiating Head Flexure and Its Effect on Transducer Performance; JASA, Raytheon S.S.D.
9. A Unique Ballistic Tunnel Measurement System; AFSC Paper describing the Aeroballistic Research Facility.
10. Aeroelastic Analysis of a Forward-Swept Wing with Stiffness Cross-Coupling. USAF.

Software Expertise
Visual Basic 6, FORTRAN 77/90, C++, UNIX, FLUENT & GAMBIT, MSC/NASTRAN, COSMOS/M, Excel, MathCAD, Photoshop, FrontPage, PDEase2D for differential equations and various CAD software packages.

AeroRocket Trademark and Copyright
The vast majority of software purchasers comply with AeroRocket's software license. Even those who have made the honest mistake of infringing on copyright or trademark have quickly corrected those mistakes when contacted. However, there are individuals or companies that after being politely contacted about copyright or trademark infringement continue to defy AeroRocket's request for compliance. Individuals who continue to defy AeroRocket copyright or trademark are listed on the Sales Banned List because of their continued defiance. The total number of individuals on this list are small but making it on this list means these individuals or companies are not eligible for software upgrades and are not permitted to benefit from AeroRocket subsonic/supersonic wind tunnel testing and consulting services.

Specific Terms of Employment Top
Please do not contact unless willing to provide a detailed position description, starting salary and starting date of employment. Otherwise, please do not waste our time with employment probes and requests for information about other potential aerospace engineering applicants.

AeroCFD® is a registered trademark of John Cipolla/AeroRocket
Copyright © 1999-2011 John Cipolla/AeroRocket