The ARDC Model Atmosphere, 1959. Appendices A thru E

Flight Test Engineering Handbook

“…Pa, inlet (atmospheric) pressure corresponding to (2) (4) tat, test atmoepheric temperature (5) tas, standard atmospheric temperature (6) at,; (4) -(5) (7) tot, test carburetor inlet temperature (8) MPt, test, instriment -corrected mnifold pressure (9) P 2 1P 1 , manifold pressure ratio, (8) + (3) (10) C, from CHART 2.32 and (7) and (9) 1i) LIMP, manifold pressure correction (10) x (8) …”

“…4't, test, instrument-corrected manifold pressure, air only stage (10) (P 2 /P')a, carburetor-deck-ambient pressure ratio, (8) …”

“…A 6273 [2][3][4][5][6][7][8][9][10][11] (i1) C, from CHART 2.31 and (10) and (4) (12) AMP., manIfold presoure correction for air only stase (11) x (9) x (6) Fuel Air Stage (13) (P2/Pl)f, manifold pressure -dock pressure ratio (9) 4 (8) (14) C, from CHART 2.32 and (13) The factors affecting pover in this case are three: the chane in carburetor temperature because of chage of free air temperature; the change of carburetor air temperature because of cbange in turbo speed; and the change In exhaust beak pressure., The equatio• for stadard horsepower under these conditions iNS The correotions in th'o equaticm are usually made empirically. First the assptions are made that the turbo does not change speed and that a change in mnifold pressure vo-1d reeslt from inlet temperature variation in going from a test day to a standard day.…”

On the effect of heavy ions on LF propagation, with special reference to a nuclear environment

“…where f(z) is the ARDC norraalized model atmospheric nnass density, [Minzner, Champion, and Pond, 1959] N^(h) is small and indeed is usually neglected. In a previous paper [Johler, 1963] [1962].…”

Effects of Nose Bluntness on the Boundary Layer Characteristics of Conical Bodies at Hypersonic Speeds

“…A technique for evaluating (14) graphically has been given by Rubin 7 to obtain the edge conditions as a function of S. With the equation in this form, real gas effects may be computed by evaluating j(y) using the real gas oblique shock relations and the real gas effects in the expansion to the inviscid cone surface. The following analysis assumes a perfect gas with…”