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

Effect of a afterbody-ejector configurations on the performance at transonic speeds[NASA TN D-1399]

By Swihart,John M,Mercer,Charles E. Washington, D.C. 1962 . 52p