Multivariate Analysis, Retrieval, and Storage System (MARS). Volume 1: MARS System and Analysis Techniques [PDF]
A method for rapidly examining the probable applicability of weight estimating formulae to a specific aerospace vehicle design is presented. The Multivariate Analysis Retrieval and Storage System (MARS) is comprised of three computer programs which ...
Hague, D. S. +2 more
core +1 more source
RESEARCH ON APPLICATIONS OF MINI-TURBOJET AND TURBOJET ENGINED MILITARY UAVS
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE, 2019 Melih Cemal Kuşhan +4 more
openaire +1 more source
Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures [PDF]
An experimental investigation was conducted to determine the cooling effectiveness of a wide variety of air-cooled turbine-blade configurations. The blades, which were tested in the turbine of a - commercial turbojet engine that was modified for this ...
Esgar, Jack B., Long, Roger A.
core +1 more source
Calculus Of Turbojet Performances For Ideal Case
, 2014 {"references": ["A. H. Lefebvre and D. R. Ballal, Gas Turbines Combustion, 3rd ed. Taylor & Francis, New York, 2010.", "J. C. Han, S. Dutta and S. Ekkad, Gas Turbine Heat Transfer and Cooling Technology. Taylor & Francis, New York, 2000.", "F. Liu and W. A. Sirignano, \"Turbojet and Turbofan Engine Performance Increases through Turbine Burners\"
S. Bennoud, S. Hocine, H. Slme
openaire +1 more source
Discussion: “The MU-CYL-JET: The Multicylinder Turbojet Engine” (Pinnes, R. W., 1962, ASME J. Eng. Power, 84, pp. 131–137) [PDF]
, 1962 Ernest C. Simpson
openalex +1 more source
Nuclear JT11D-20 Turbojet Engine Estimated Performance 1800F NaK Radiator
, 1960 J. W. Larson
openalex +4 more sources
Experimental cold-flow evaluation of a ram air cooled plug nozzle concept for afterburning turbojet engines [PDF]
A concept for plug nozzles cooled by inlet ram air is presented. Experimental data obtained with a small scale model, 21.59-cm (8.5-in.) diameter, in a static altitude facility demonstrated high thrust performance and excellent pumping characteristics ...
Harrington, D. E., Straight, D. M.
core +1 more source
HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1 [PDF]
, 1965 HILLER AIRCRAFT CORP PALO ALTO CA
openalex +1 more source
Optimization and guidance of flight trajectories for the national aerospace plane [PDF]
The research on optimal trajectories for the National Aerospace Plane (NASP) performed by the Aero-Astronautics Group of Rice University from June 22, 1989 to December 31, 1990 is summarized.
Miele, Angelo
core +1 more source
Effect of shocks on film cooling of a full scale turbojet exhaust nozzle having an external expansion surface [PDF]
, 1979 David M Straight
openalex +1 more source