EFFECT OF AFTERBODY-EJECTOR CONFIGURATIONS ON THE PERFORMANCE AT TRANSONIC SPEEDS OF A PYLON-SUPPORTED NACELLE MODEL HAVING A HOT-JET EXHAUST

By Swihart,John M, Mercer,Charles E. Nasa, Washington, D.C. 1959 . 53 , Bound With Nasa Memo 1-2-59l-1-10-59l

SUBSONIC PERFORMANCE CHARACTERISTICS OF A LARGE-SCALE 1.075-PRESSURE-RATIO TIP-TURBINE CRUISE-FAN PROPULSION SYSTEM

By Capone,Francis J. Nasa, Washington, D.C. 1969 . 276 , Bound With Nasa Tn D-5311-20