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Antigravity - Buffer Zone "Aerodynamics" [1] Part One "Modifying the gravitational field with electrogravitics, a continuous streamline pattern (buffer zone) is obtained at supersonic speeds, even with the B-2's [2] smooth airfoil design. This compares favourably to flying disks. That is, the approach flow is able to sense the presence of the B-2. In terms of 100 % antigravity (e.g., ET-crafts), the approach flow is seemingly able to sense instantaneously the oncoming craft." Stealth - Additional Note /J.R.C. The high stagnation-pressure losses in the bow shock wave at supersonic speed is one important reason, among several others [3], to employ the more efficient electrogravitics or antigravity operable propulsive systems. With electrogravitics or antigravity repulsive force field no energy is dissipated as shock or sound wave [4]. The uniform flow forms a stream surface with a geometric pattern approximating the shape of the craft [5]. According to conventional aerodynamic theory, a moving craft will cause pressure waves to propagate through the surrounding fluid at the local speed of sound. The zone of influence i.e., the zone where the approach flow is aware of the presence of the craft varies with speed. At supersonic speed, shock waves form where the local pressure, velocity and entropy abruptly change. Behind the shock wave, the craft resumes direct influence upon the ambient flow. With antigravity; a negative energy (local spacetime curvature) EM field accelerates the craft. A continuous streamline pattern, without bow or trailing shockwaves, is created instantaneously around the craft. The information to "flow around the craft without air compression or expansion" arises from the force field lightspeed impulses in 4-space [6]. In this constant-pressure subsonic laminar flow, the random molecular motion is minimal. There are no separated flow regions or stalling of the air. No drag force is acting on the craft, inasmuch as all pressure coefficients are in sync with the shape of surface. It may now be understood why, on the outskirts of the buffer zone, some speedier molecular motion necessarily may drift into the slower region of flow. In this subsonic diffusion zone there is an effect of kinetic energy storage where supersonic flow enters smoothly. Through the pressure signalizing system the energy is diverted back on schedule to the initial flow pattern. The ramification is a "buffer zone" which we observe macroscopically as a well-ordered laminar flow region around the craft. [1] Not to be mistaken with the buffer layer, a region found within a turbulent boundary layer (see boundary layer theory). Antigravity, ignored by the mislead scientific community. Revolutionary propulsion technologies have long been the focus of a super secret well-conceived scientific effort. [2] All 21 Northrop Grumman B-2 stealth bombers are expected to see service end around 2060 (!) [3] Benefits such as: In flight g-forces (acceleration, sharp turns, etc.) on craft and crew are eliminated. No aerodynamic heating. [4] A rounded leading edge on conventional aircrafts induces a detached shock. The shape of the wave and the shock-detachment distance are dependent on the Mach number and aircraft profile. [5] To encourage laminar flow (less drag) the common practice is to shape the airfoil with a concave lower surface at the trailing edge and a convex upper surface with a large lift region of supersonic flow. [6] A local spacetime/gravitational field is surrounding the craft. 4-space: length cubed multiplied by time. Distinct from the mental picture of a merging of space and time. With a curved spacetime the 3-space energy symmetry is dismissed. Einstein made allowance for the attraction of mass only. He did not firmly adhere to the linking of electromagnetism and gravitation when considering the distortion of the local spacetime metric. Suggested readings: T. E. Bearden, Energy from the Vacuum: Concepts and Principles, Cheniere Press, Santa Barbara, CA, 2002. http://xxx.lanl.gov/abs/hep-th/9901011
Jan Riis-Christensen 2004-10-20
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