02474oam 2200709 450 991071601930332120210601100647.0(CKB)5470000002517915(OCoLC)23295306(OCoLC)760971134(EXLCZ)99547000000251791519910326j197212 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration /by Louis E. ClarkWashington, D.C. :National Aeronautics and Space Administration,December 1972.1 online resource (52 pages) illustrationsNASA/TN ;D-7060"December 1972."Includes bibliographical references (page 10).Aerospace vehiclesnasatAerodynamicsnasatSpace vehiclesAtmospheric entryLeading edges (Aerodynamics)Aerodynamic heatingAerothermodynamicsSpace shuttlesAerodynamic heatingfastAerothermodynamicsfastLeading edges (Aerodynamics)fastSpace shuttlesfastSpace vehiclesAtmospheric entryfastAerospace vehicles.Aerodynamics.Space vehiclesAtmospheric entry.Leading edges (Aerodynamics)Aerodynamic heating.Aerothermodynamics.Space shuttles.Aerodynamic heating.Aerothermodynamics.Leading edges (Aerodynamics)Space shuttles.Space vehiclesAtmospheric entry.Clark Louis E.1419962United States.National Aeronautics and Space Administration,ABCABCAD#OCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOBOOK9910716019303321Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration3536156UNINA