Mayes, H.William
NASA technical note [D21-30] : Near-field and far-field noise surverys of solid-fuel rocket engines for a range of nozzle exit pressuress / NASA .- National aeronautics and space administration : NASA, 1959 .- 32p.
TR8550 : [D-22] Measurement of ground -reaction forces and vertical acceleration at the center of gravity of a transport airplane taxiing over obstacles by James M. Mckay.
TR8551 : [D-23] Experimental operating performance of a single-stage annular air ejector by Robert R. Howell.
TR8552 : [D-24] Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones by Briggs benjamin R.
TR8553 : [D25] Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing four propellers and blowing flaps by Weiberg, James A.
TR8554 : [D-26] Moving-cockpit simulator investigation of the minimum tolerable longitudinal maneuvering stability by Brown, porter B.
TR8555 : [D-27] Shielding stagnation surfaces of finite catalytic activity by air injection in hypersonic flight by Chung, paul M.
TR8556 : [D-28] A combind water-bromotrifluoromethane crash-fire protection system for A T-56 turbopropeller engine by Campbell, john A.
TR8557 : [D-29] Summary of veg and V-G data obtained from 1947 to 1958 by Walker, Walter G.
TR8558 : [D-30] Flight investigation of the lift and drag characteristics of a swept-wing multijet transport-type airplance by Tombor Ronald
Subject Headings:
Nasa technical note;
Author Added Entry:
Landford, H.Hubbard;
Hubbard, H. Harvey;
Copy Details:
Acc. No.: 63628, Full Call No.: NASA-TN-D-21-30, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
------------------------- --------------------- ------ --------- ------- ------- --------- --------
NASA technical note [D21-30] : Near-field and far-field noise surverys of solid-fuel rocket engines for a range of nozzle exit pressuress / NASA .- National aeronautics and space administration : NASA, 1959 .- 32p.
TR8550 : [D-22] Measurement of ground -reaction forces and vertical acceleration at the center of gravity of a transport airplane taxiing over obstacles by James M. Mckay.
TR8551 : [D-23] Experimental operating performance of a single-stage annular air ejector by Robert R. Howell.
TR8552 : [D-24] Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones by Briggs benjamin R.
TR8553 : [D25] Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing four propellers and blowing flaps by Weiberg, James A.
TR8554 : [D-26] Moving-cockpit simulator investigation of the minimum tolerable longitudinal maneuvering stability by Brown, porter B.
TR8555 : [D-27] Shielding stagnation surfaces of finite catalytic activity by air injection in hypersonic flight by Chung, paul M.
TR8556 : [D-28] A combind water-bromotrifluoromethane crash-fire protection system for A T-56 turbopropeller engine by Campbell, john A.
TR8557 : [D-29] Summary of veg and V-G data obtained from 1947 to 1958 by Walker, Walter G.
TR8558 : [D-30] Flight investigation of the lift and drag characteristics of a swept-wing multijet transport-type airplance by Tombor Ronald
Subject Headings:
Nasa technical note;
Author Added Entry:
Landford, H.Hubbard;
Hubbard, H. Harvey;
Copy Details:
Acc. No.: 63628, Full Call No.: NASA-TN-D-21-30, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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