DOCSLIB.ORG
Explore
Sign Up
Log In
Upload
Search
Home
» Tags
» Kholod
Kholod
Aeronautical Engineering
Overview of Nato Background on Scramjet Technology
Research Training Group Grk 1095/1: "Aero-Thermodynamic Design of a Scramjet Propulsion System"
1.Russian Information Weapons; 2.Baltic Department of Defense, Or the US Defenses (Estonia, Latvia, Lithuania) Against Government
Large Eddy Simulation of Turbulent Supersonic Combustion and Characteristics of Supersonic Flames
Recent Flight Test Results of the Joint CIAM- NASA Mach 6.5 Scramjet Flight Program
Trends in Satellite Earth Observation for Permafrost Related Analyses—A Review
Reduced-Order Analysis of Dual Mode Supersonic Combustion
The Inverse Design of Hypersonic Flow Paths
The Air and Space Sale I New York I September 17, 2019 25262
The Global Methane Budget 2000-2017
Hypersonics: Past, Present, and Potential Future
A REVIEW on HYPERSONIC AIRCRAFT Khedkar Sudesh B .1,Kasav Sayali M.2,Khedkar Aniket S.3, Mahajan Sunil M4, Satpute Dinesh R5 1,2,3, U
Future Flight Test Plans of an Axisymmetric Hydrogen-Fueled Scramjet Engine on the Hypersonic Flying Laboratory
PROPULSION SYSTEMS for HYPERSONIC FLIGHT 1. Introduction
Accelerating Methane Growth Rate from 2010 to 2017: Leading Contributions from the Tropics and East Asia
Chiesa Ortodossa Russa
A Performance Analysis of a Rocket Based Combined Cycle (RBCC) Propulsion System for Single-Stage-To-Orbit Vehicle Applications
Top View
A Survey of Gaps, Obstacles, and Technical Challenges for Hypersonic Applications
Accelerating Methane Growth Rate from 2010 to 2017: Leading Contributions from the Tropics and East Asia
Ramjet and Dual Mode Operation
As Ferramentas Da Política Energética Externa Da Rússia Para a União Europeia
ANNUAL REPORT 2017 / 18 Our Growing Commitment to a Sustainable Future Research and Outreach Activities in Over 50 Countries
The Emissions Gap Report 2017 a UN Environment Synthesis Report
The Global Methane Budget 2000–2017
Correcting Model Biases of CO in East Asia
A Preliminary Design of Flight Test Conditions for a Sub-Scale RBCC Engine Using a Sounding Rocket
Recent Flight Test Results of the Joint CIAM- NASA Mach 6.5 Scramjet Flight Program