- 108 -

Allen, D. J.: The Application of b~ulthopp's Subsonic Lifting Sur-
  face Theory to the Calculation of %he Aerodynamic Forces )%cting
  on a Wing of Finite Aspect Ratio Oscillating in Arbitrar~ ~l~ic
  Modes With Control $:Lrface Freedom. Design Dept. Rep. No. ll91,
  Hawker Aircra£t, Ltd. [Kingston-on-Thames, England], June 1953.

D. ?'Y (~e G. Allen and R.V.                      " ]lelaxation methods applied to cletennine the motion, in two dimensions, of
   ,outil~'elt                                    a viscous fluid i~.~'t~..d cylinder. Quart. J. Mech. App. Math. II1.

                       •                               Part 2. June, 1~55.                    "                                      •

       tt Allen. F. J., An "EJasllc-J'lasti¢ Thecfy~af..Jhe Respo,se of
        Cantilevers to A ie Blast Loadi.r, BRL M R~. ti~.~pri11955.

  Allen, g. J. : General Theory of Airfoil Sections ~ving arbitrary Shape
  or Pressure Distribution. NACA Tech. Rept. No. 853, 1947. | 26 6
        t, Allen. H. Julian. Prexsure Distribution a,~d SO,he Efftcts of
        Viscosity on Sle~dcr lndincd Bodies of Ret,ohdion, N.A.C.A.T.N.                     / I ~ 7
        No.2044. m~. I 9 2 1

  Allen, H. Julian: Motion of a Ballistic ~tlssi!e Angularly Misaligned
   Wlth the Flight Path Upon Entering t.he Atmosphere and Its Effect
   Upon Aerodynamic Heating, Aerodynamic Loads, and Miss Distance
   NACA ~ 4048, 19.57. 2 O0 1

        4. Allen, H. J,Iian: A Simplified .Met~,(~l ~:~rAhc C,deu',ati ....            fair-
        foi! l'red, tire l)i~tributiun. NA(tA¢I'K .'~o. 76S, 1939.

   3. Allen, H. Julian: gstimation of the Forces and Mc~.ents Acting on
        Inclined Bodiesel    ~v~lutlon            of    High Fineness Ratio. NACA
        I~ A9126, 1949.




~. Allen. 11. J,llhm: Calculalioh .,f the Ch(,rdwi.,. l.,*a,l Di-!ril.ll.*n
   m't.r Airfoil .'h.,:ti,,n, with Phd,*. :';Ill)t. ,~.l~qially lli;.g..d
   'fraili,~x-l'hb4o i"lnl~S. N.%.(:.~. Ile],. N,,." 6~, I:k~.

     " Alle., II. J., "llyper~nnie. flight and the re-entry probiem,"
  .I. A~,,m,,,~ s~i. as, 217-'22~ (l,SS)2 I e~ 8 "                                 f 549-
Allen, H. Julian, mid Eggers, A. a., Jr.: A Study oe the Notion ani"ilO7l,aTl~'l~l~*lTl~
                                         . bl/o@,aal~ ,tqeZ Z37~
     Aerodynamic Heating of Missiles Enterir, the Earth's Atmosphere a~i~it;*7,'~'b,
     High Supersonic Speeds. NACA 'l'TT ~047, 1,957.     ~,b 3

     Various lli~hly Rc.ctit,e Puds in . :~.v'l-i'.v-I° i,~, 1~ .'Ja~ h 2 II',,:d
     T,,,,d. NASA MF.MO 1-15-591.L ~ ~ & C)

H. J. "~-len,                                    'ihe ~.ntoraction of boundary layer and                                                              _/'~""'~/,
~I. A. IIeaslet and compressicn ~hock anal its effect ~                                                l~') 70
G. E. Nitzberg airfoil prezsuu-e distrib~t~/7~
                                                 N.A.C.A..~C X7.~02 (~947). " "~

                                        I
• Allen, ~. Julian, and N1tzl~rg, Gerald E. : The Effect, of Comgresel-
   blllty on the Growth of t}~e L~mlaar Bo~dary Layer on Low-Drag       I
  Wings and Bodies. NACA ACR, Jan. 19~3 ~ 0 7 ~

      8. ^m,,,, 'i'.-at,li'~,,,,'a, tdP,~r|,i,,,,,';,i,,'drdW.:,\S,.a;:'i,}~i~o',.;;r ......        /~'27 1/-/~,5 ~373 ~)
            of ViscoMty on the Flow Ovnr Slender hwlhu,d Bodic~ nf Revo.
          lull ....NA~/~ ~e.~ 10'18, 1114%1. (S,l .....     1,', NAC.A 'rN           /I.t.b~,     iI~blt. 122g
                                                                                                                           EL..>
            20,14.)

 Allen, H. Julian, and Perkins, Edward W. : Characteristics of Flow
      Over Inclined Bodies of Revolution. NACA RM ASOL07, 19~i. if ~ $ ~/

     1~, H. J. AL'I,EN and-~,V.'Ql.Vlff0g~q'rl ;-"'Wall Interference       1711#
                 in a Two.])imensional I,'l.w Wind Tmmd, with Con-
               sidemtioJt of tho Effect of Coml.c~sibility," N.A.C.A.,                      IgO3
                                                                                                            v:i2_~
                 T.IL. 782 (1914). " -£ 2

    14 Allen, R.A., Keck, J.C. and C~.m, J.C., "The Recombination
   of Nitrogen at 614-00 K, "Ayes-Everett Research Lab., Research
   No~e 21~3, .June 1961. I 5 ~12



FIGURE 7. I                   CITATION INDEX SHEET