Vehicles that operate in air and vacuum, where mass budgets are brutal.
14 topics · 16 curated works
No prior grounding assumed.
The Wright Brothers' Aëroplane
Orville Wright & Wilbur Wright · 1908
The Wrights' own account of the reasoning behind their aircraft's design — three-axis control through wing-warping linked to the rudder, and a…
Assumes you know the vocabulary.
Origins of Inertial Navigation
Charles Stark Draper · 1981
Traces inertial navigation from a laboratory curiosity to the system that guided submarines and spacecraft, arguing its central problem was never the…
+2 more at this level
Primary sources and full treatments.
Motion of Fluids with Very Little Viscosity
Ludwig Prandtl · 1904
Argues that viscous effects in a fast-moving fluid are confined to a thin boundary layer near the surface, so drag and separation can be analysed…
+11 more at this level
12 of 16 works
Orville Wright & Wilbur Wright
The Wrights' own account of the reasoning behind their aircraft's design — three-axis control through wing-warping linked to the rudder, and a deliberately unstable airframe that made that control effective — laying out a design logic every conventional aircraft since has inherited.
about 55 minutes to readlink checked 17 Sept 2026Charles Stark Draper
Traces inertial navigation from a laboratory curiosity to the system that guided submarines and spacecraft, arguing its central problem was never the physics of the gyroscope but building instruments precise enough to trust without an external reference.
Columbia Accident Investigation Board
Argues that the foam strike was the proximate cause and NASA's own culture the real one: repeated anomalies had been reclassified as acceptable until the organisation could no longer hear a warning.
Federal Aviation Administration
Works through how a gas turbine engine's compressor, combustor and turbine sections interact to produce thrust, and how each is inspected and maintained, as the standard reference used to certify the technicians who keep them running.
Ludwig Prandtl
Argues that viscous effects in a fast-moving fluid are confined to a thin boundary layer near the surface, so drag and separation can be analysed there while the outer flow is treated as inviscid.
link checked 17 Sept 2026George H. Bryan
Derives the equations of motion of an aeroplane from rigid-body dynamics and shows that stability is a property of the characteristic roots of the linearised system, founding flight dynamics as an analytical discipline rather than a matter of pilot skill.
link checked 17 Sept 2026Theodore Theodorsen
Derives a closed-form unsteady aerodynamic theory for an oscillating airfoil and uses it to give the first general criterion for flutter onset, founding aeroelastic analysis as a predictive discipline rather than a matter of post-hoc accident investigation.
link checked 17 Sept 2026Ira H. Abbott, Albert E. von Doenhoff & Louis S. Stivers Jr.
Compiles wind-tunnel-measured lift, drag, pitching-moment and pressure-distribution data across the whole family of NACA airfoil sections into one reference, so a designer can select a section from measured behaviour rather than testing a new one from scratch.
National Advisory Committee for Aeronautics
Reduces every one-dimensional compressible-flow problem — normal shocks, isentropic expansion, Rayleigh and Fanno flow — to a common set of tables so an engineer need not re-derive the gas-dynamic equations by hand each time.
link checked 17 Sept 2026George Gerard & Herbert Becker
Collects buckling solutions for flat plates and stiffened panels under combined loading into standard design curves, turning aircraft structural stability from a case-by-case elasticity problem into a lookup procedure.
link failing as of 17 Sept 2026H. Julian Allen & A. J. Eggers Jr.
Shows that a blunt nose, not a sharp one, minimises the heat transferred into a body re-entering the atmosphere at hypersonic speed, because a detached bow shock deflects most of the kinetic energy into the surrounding air rather than the vehicle — the insight behind every capsule shape since.
link checked 17 Sept 2026Dieter K. Huzel & David H. Huang
Lays out the complete engineering design sequence for a liquid rocket engine — combustion chamber, injector, turbopump, cooling — as practised at Rocketdyne, treating rocket engine design as systems engineering under extreme thermal and structural loads.
This subject genuinely sits in more than one domain. These fields approach the same ground with different methods.