C.P.  / 582 <br/>
Lawlor,E F <br/>
       WIND TUNNEL TESTS AT MACH NUMBERS BETWEEN 0.6 AND 1.4 OF A 60 DEGREE SWEPT WING HAVING AN AEROFOIL SECTION DESIGNED FOR SUBCRITICAL FLOW AT A MACH NUMBER OF 1.2 
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 .-  Her Majesty'S Stationery Office, London,  1962 
<br/>Bound With C.P.581, 583-590 
<br><U>Copy Details:</u><br> Acc. No.: <b>TR10471</b>, Full Call No.: C.P. 582,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>