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Mathematical models
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models
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keywords:(Mathematical models)
A Mamathematical Approach for Optimum Checkout Design Criteria
Discussion of the Fault and Dike Problems in Magnetotelluric Theory
Research, Development, and Testing of Underwater Propulsion Devices
Stability of Tapered Rectangular Plates under Varying Compression and Shear Loads
An Investigation of the Jetevator as a Means of Thrust Vector Control
The Variation of Heating Rates in a 1/30 Scale Booster Rocket Exhaust Jet
Analysis and Evaluation of Supersonic Underwing Heat Addition
An Analysis of Emergency Airlift
PERFORMANCE AND DESIGN CRITERIA OF AN ADAPTIVE CIRCUIT PROPOSED FOR A SPACE RE-ENTRY VEHICLE
Some Static Aeroelastic Considerations of Slender Aircraft
The Kiting Motion of a Masted Airship as Determined by Analytic Evaluation of Water Model Tests
Selection of Upper Stage Propulsion Systems for Space Vehicles
Application of Analytical Techniques to Flight Evaluations in Critical Control Areas
The Influence of Compression Ratio and Dissociation on Ideal Otto Cycle Engine Thermal Efficiency
Empirical Evaluation of Powerplant Dynamics for Computer and Field Performance Monitor Applications
The Model-Controlled Method for the Development of Variable-Stability Aircraft
Ordnance Engineering Design Handbook. Surface-to-Air Missile Series. Part Two. Weapon Control
A Portable Passive-Element Network Analyzer for Engineering Systems Simulation
SIMULATION MODELS FOR SPACE LOGISTICS ANALYSIS
Simulation Approach to Development of the XV-5A Lift-Fan V/STOL Aircraft
Simulation of Helicopter and V/STOL Aircraft., Volume I: Helicopter Analysis Report
Linear Acceleration Guidance for Lunar Landing and Launch Trajectories
Application of the Matched Conic Model in the Study of Circumlunar Trajectories. Project APOLLO
Electrical Strain Producers in Flight Control Applications
Highway Travel in Washington, New York, Boston Megalopolis
Flight Hazard Analysis for SNAP Payload
A Projection of Planning Factors for Land Use and Transportation
Studies to Determine Optimum Lunette Load for the Lance Lightweight Launcher