Synonyme wurden verwendet für:
HYPERSONIC
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HYPERSONIC SPEED
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SPEED
Suche ohne Synonyme:
keywords:(HYPERSONIC SPEED)
Boundary-layer transition on a film-cooled slender cone
DebrisLV Hypervelocity Impact Post-Shot Physical Results Summary
Hyperschallversuche bei hoher Gleitzahl und Klappenerwaermungsuntersuchungen
Hypersonic Aerodynamics Fellowships
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - MIDAS Development & Demo
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Key Findings Detailed
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
Second Law Approach to Aircraft Conceptual Design
Determination of Three-Dimensional Flow Separation by a Streamline Method
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
Effects of Surface Emittance on Turbulent Skin Friction at Supersonic and Low Hypersonic Speeds
Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers
Hypersonic Weapons Technology for the Time Critical Mobile Ground Threat A State-of-the-Art Review
State-of-the-ART Study for High-Speed Deceleration and Stabilization Devices Final Report
Hypersonic and Unsteady Flow Science Issues for Explosively Formed Penetrator Warheads
Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations
Design of the Phoenix Missile Hypersonic Testbed (PMHT)
Supersonic Investigation of Two Dimensional Hypersonic Exhaust Nozzles
Leeside Separation of Hypersonic Weapons
Lift-to-drag ratios of slender wings at hypersonic speeds
Maximum lift-to-drag ratios of a slender, flat-top, hypersonic bodies, part 1
Debris Production in Hypervelocity Impact ASAT Engagements
Chief Engineer's View of the NASA X-43A Scramjet Flight Test
Entropy Wake Behind a Sphere in Hypersonic Flight
New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems
Environmental Assessment for Hypersonic Technology Vehicle 2 Flight Tests
Lift-TO-Drag Ratios of Slender Wings at Hypersonic Speeds
Dynamics of Debris Motion and the Collision Hazard to Spacecraft Resulting from an Orbital Breakup
One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool
Engineering the Space Age: A Rocket Scientist Remembers