Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
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 - Key Findings Detailed
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
State-of-the-ART Study for High-Speed Deceleration and Stabilization Devices Final Report
Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations
Design of the Phoenix Missile Hypersonic Testbed (PMHT)
Supersonic Investigation of Two Dimensional Hypersonic Exhaust Nozzles
Lift-to-drag ratios of slender wings at hypersonic speeds
Maximum lift-to-drag ratios of a slender, flat-top, hypersonic bodies, part 1
Chief Engineer's View of the NASA X-43A Scramjet Flight Test
New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems
Entropy Wake Behind a Sphere in Hypersonic Flight
Lift-TO-Drag Ratios of Slender Wings at Hypersonic Speeds
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
One-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
Maximum Lift-TO-Drag Ratios of a Slender, Flat-Top, Hypersonic Bodies, Part 1
An Experimental Investigation of the NASA Space Shuttle External Tank at Hypersonic Mach Numbers
X-15: Extending the Frontiers of Flight
Air Intakes for a Mach 7 Aircraft
Airbreathing Hypersonic Vision-Operational-Vehicles Design Matrix
Aerodynamic Stability and Control Characteristics of Tbc Shuttle Booster AR-11981-3
Flow-Field Investigations on the X-15 Airplane and Model Up to Hypersonic Speeds
Analysis of the project fire re-entry package flow field final technical report
One-Dimensional Approach to the Maximum Lift- TO-Drag Ratio of a Slender, Flat-Top, Hypersonic Wing