Base flow/underexpanded exhaust plume interaction in a supersonic external flow
Base Flow/Underexpanded Exhaust Plume Interaction in a Supersonic External Flow
Effects of flow and geometry parameters on shock-wave boundary-layer interaction phenomena
Effects of Flow and Geometry Parameters on Shock-Wave Boundary-Layer Interaction Phenomena
Ramjet Engine Test Facility (RJTF) in NAL-KRC, Japan
Ramjet Engine Test Facility (RJTF) in NAL-KRC, Japan
Design and testing of 2-D fixed-geometry hypersonic intakes
Design and Testing of 2-D Fixed-Geometry Hypersonic Intakes
Flight dynamics and robust control of a hypersonic test vehicle with ramjet propulsion
Flight Dynamics and Robust Control of a Hypersonic Test Vehicle with Ramjet Propulsion
Experimental analysis of the flow of exhaust gas in a hypersonic nozzle
Experimental Analysis of the Flow of Exhaust Gas in a Hypersonic Nozzle
The FESTIP Technology Development and Verification Plan
The FESTIP Technology Development and Verification Plan
Accuracy of AUSM+ scheme in hypersonic blunt body flow calculations
Accuracy of AUSM+ Scheme in Hypersonic Blunt Body Flow Calculations
Some numerical investigation results of shock-induced combustion
Some Numerical Investigation Results of Shock-Induced Combustion
Performance of Centrospazio Hypersonic High Enthalpy Wind Tunnel
Performance of Centrospazio Hypersonic High Enthalpy Wind Tunnel
Development of a CMC-based TPS for two representative specimens of cryogenic tank RLVs
Development of a CMC-Based TPS for Two Representative Specimens of Cryogenic Tank RLVs
Hydrocarbon fueled scramjets for hypersonic vehicles
Hydrocarbon Fueled Scramjets for Hypersonic Vehicles
Scramjet combustor design in French PREPHA program - Final status in 1998
Scramjet Combustor Design in French PREPHA Program - Final Status in 1998
A model based control system for the Scirocco plasma wind tunnel
A Model Based Control System for the Scirocco Plasma Wind Tunnel
Oblique detonation wave studies in the Caltech T-5 Shock Tunnel Facility
Oblique Detonation Wave Studies in the Caltech T-5 Shock Tunnel Facility
A simple analytical model for parametric studies of hypersonic waveriders
A Simple Analytical Model for Parametric Studies of Hypersonic Waveriders
Measurements of scramjet engine performance by gas sampling
Measurements of Scramjet Engine Performance by Gas Sampling
Simulation tests for investigating flying qualities of aerospace planes
Simulation Tests for Investigating Flying Qualities of Aerospace Planes