AeroRocket Engineering

Providing Affordable Aerodynamics Software Since November 1, 1999





Latest Publications
Ring Fin Rocket Center of Pressure, Drag and Lift Slope Coefficients
Measured Using the AeroRocket Wind Tunnel, Technical Note 2022-2 (2022)

Spool Rocket Center of Pressure and Drag Coefficient Measured
Using the AeroRocket Wind Tunnel, Technical Note 2022-1 (2022)

Warp Drive Propulsion Using Magnetic Fields to
Distort Space-Time OR
First Successful Warp Drive Flight (2021)

POF 291 Flutter Velocity Error Produces Negative Margins of
Safety Compared to NACA TN 4197, Technical Note 2021-2 (2021)

FinSim 10 Torsional Stiffness of Rocket Fins
Thickness-Tapered From Root to Tip, Technical Note 2021-1

"Proving Shock Thickness Decreases for
Increasing Mach Number", Shock Wave Thickness Analysis, (2020)

"Demonstrating the Relationship Between
Quantum Mechanics and Relativity", Theory of Everything, (2019)

Experimental Rocket Launches
Micro-vehicles Launched on Jets of High Velocity Water
HTV-3X Space Plane Development

Sprint Experimental Rocket

Sprint Model Rocket

AeroRocket specializes in subsonic, supersonic and hypersonic aerodynamics, Computational Fluid Dynamics (CFD), warp drive physics and aerospace related software development for rockets, airplanes and gliders. Other services include wind tunnel testing using the AeroRocket designed and fabricated subsonic wind tunnel and supersonic blow-down wind tunnels.

AeroCFD is a registered trademark of John Cipolla and is classified as an axisymmetric 3-D and planar 2-D Computational Fluid Dynamics (CFD) computer program. However, AeroCFD solutions are not limited to bodies of revolution even though AeroCFD's bodies of revolution can be very complex.

John Cipolla
Chief Aerodynamicist,
AeroRocket and WarpMetrics

Impeach Joe Biden the 46th President of the United States
for not Defending and Protecting the U.S. Constitution and not
Protecting the Southern Border of the United States From Invasion

Joe Biden violated his oath of office as President of the United States when he boldly declared freedoms expressed in the Constitution are not absolute. The following well documented comment makes President Biden unfit for office and explains his total disregard and contempt for Americans basic right of free speech and the right to keep and bear arms guaranteed by the United States Constitution.

'No amendment to the Constitution is absolute'
President "Brandon" Biden
April 8, 2021

The Presidential Oath of Office

I do solemnly swear (or affirm) that I will faithfully execute the Office of President of the United States, and will to the best of my Ability, preserve, protect, and defend the Constitution of the United States.

The Constitution of the United States, Article II, Section 1


Nozzle 10: One-dimensional and two-dimensional, compressible flow computer program for the analysis of converging-diverging nozzles, including ramjet and scramjet engines. Nozzle models inviscid, adiabatic and hence isentropic flow of a calorically perfect gas through variable-area ducts. Nozzle internal flow may be entirely subsonic, entirely supersonic or a combination of subsonic and supersonic including shock waves in the diverging part of the nozzle. Shock waves are clearly identified as vertical red lines on all plots. Nozzle 3.7 Copyright  John CipollaThe cross-sectional shape in the axial direction of the nozzle is specified by selecting from five standard nozzle types or by defining nozzle geometry using the Free-Form nozzle geometry method. Nozzle plots color contours of pressure ratio, temperature ratio, density ratio, and Mach number and has a slider bar that displays real-time values of all nozzle flow properties. New in this version is the ability to determine shock-angle, jet-angle (plume-angle) and Mach number for axisymmetric and two-dimensional nozzles in the region near the lip for underexpanded and overexpanded flow. The converging-diverging nozzle featured in the new AeroRocket supersonic blow-down wind tunnel was designed using Nozzle applying the concept of a normal shock diffuser. More ...

HyperCFD 10
: Supersonic and hypersonic re-entry vehicle and rocket analysis computer program based on advanced principals of 3-D Gasdynamics. HyperCFD, determines drag coefficient (Cd), center of pressure (Xcp), CN-alpha and Cm-alpha of supersonic and hypersonic rockets and re-entry vehicles. In addition, on a separate screen HyperCFD displays and plots CN-Body, CN-Fins, CN-Total and Cm-Total as a function of angle of attack (AOA) using up/down controls. HyperCFD uses empirical aerodynamic corrections to the modified Newtonian surface inclination method that allows excellent results from Mach 1.05 to Mach 20. Includes a wide variety of nose cone shapes and fin cross-sections. Nose cone shapes include, conical, elliptical, parabolic, power series Sears-Haack, tangent ogive and spherical segment. Fin cross-sections include single wedge, symmetrical double wedge, arbitrary double wedge, biconvex section, streamline section, round-nose section, and elliptical section fin shapes. HyperCFD is useful to determine supersonic and hypersonic rocket drag and center of pressure location for medium and large scale professional sounding rockets. Finally, HyperCFD 10.xx models hypersonic glide vehicle (HGV) aerodynamics. More ...

FinSim 10, Flutter Velocity Tool: Quickly and easily predict fin flutter velocity, UF and fin divergence velocity, UD for any rocket while specifying fins in the Fin Geometry screen by simply using a slider bar. Predict flutter velocity from sea level all the way to maximum altitude that was defined on the main AeroFinSim analysis screen. Get instant flutter velocity feedback while specifying fin geometry and get an idea of fin shock angle and fin Surface Mach number that a fin will experience during supersonic flight. Flutter velocity accuracy is enhanced by using the NASA web site atmospheric model that predicts free stream pressure (P) temperature (T), density (r)and speed of sound as a function of altitude from sea level while flying through the Troposphere (h < 36,152 feet), Lower Stratosphere (36,152 feet < h < 82,345 feet) and finally the Upper Stratosphere (h > 82,345 feet). The atmospheric model used in FinSim is not limited to only the Troposphere or 36,152 feet. More ...

Special Links
    Magnetic Levitation Warp drive analysis
Magnetic Levitation and
 Warp Drive propulsion
AeroRocket References
Reference Books
Enclosed flow lift analysis
Ducted Wing and VASIMR
Plasma Rocket Propulsion
X-30 NASP AeroWindTunnel analysis
SS1 wind tunnel testing
HTV-3X wind tunnel tests

Some Validation Analyses

Shock Thickness | AeroSpike Validation | Nozzle Validation (1) | Nozzle Validation (2)
AeroCFD V-2 Analysis | AeroCFD Cone-Cylinder Analysis | SS1 Spaceplane Analysis | Rocket Center of Pressure
Companies that use AeroRocket Software

Additional Links
Contact John Cipolla
Contact AeroRocket
Kenneth Bailey and Paul Latshaw Attack UFO

Software Comments

Trump Calls for Boycott of Select Marxist Companies!
Major League Baseball, Delta Airlines, Coca Cola, JPMorgan Chase,
Viacom CBS, Citigroup, Cisco, UPS and especially DirecTV/AT&T
for silencing One America News and other conservative voices

Socialist-Marxist Companies Conservatives Should Boycott
Good Companies Conservatives Should Support


BOMBSHELL: Biden Family Scored $31 Million from Deals with Individuals with Direct Ties to the Highest Levels of Chinese Intelligence. According to news reports, President Biden is compromised by the Chinese Communist Party (CCP).


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AeroCFD is a registered trademark of John Cipolla/AeroRocket
Copyright 1999-2022 John Cipolla/AeroRocket & WarpMetrics
Site updated 01/27/2022