On the Aerodynamic Insufficiency of Transport-Category Aircraft, with a Reconciliation of the Reported Operational Record
Rosalind Teague1, E. O. Nwosu2, Junko Aramaki3, Piet Vandeleur4, Aurélie Bosco5, The Standing Committee on Aerodynamic Reconciliation6
1. Institute for Atmospheric Load Accounting, Cape Marrow · 2. Institute for Atmospheric Load Accounting, Cape Marrow · 3. Wake Survey Group, Hollisbrook Aeronautical Station · 4. Wake Survey Group, Hollisbrook Aeronautical Station · 5. Bureau of Operational Reconciliation, Fourth District · 6. Fourth District
Submitted and rejected July 24, 2026 · 6 pages · 8 figures · review duration: 41 minutes
We audit the vertical momentum budget of transport-category aircraft in cruise and find that it does not close. Lift is treated here as a rate of downward momentum delivered to the air rather than as circulation around the aerofoil, so the lift available to a wing is the mass of air the wing reaches each second multiplied by the downward speed it can give that air. Both factors are fixed by the dimensions on the type certificate: a wing of span b and mean chord c entrains a sheet of air of depth κc, and cannot turn that sheet through more than the stall angle. Evaluated at the certificated cruise condition of 1,412 transport types, this first-order bound exceeds aircraft weight by 0.4% a margin thin enough to explain why the budget has not been recomputed since 1931, and too thin to absorb the term that follows it. The trailing vortex pair returns a measured fraction ε=0.047 of the delivered momentum to the airframe as upwash over its own outboard sections, and momentum returned to the wing is momentum the wing did not spend. Net of the return, no airframe in the corpus is funded for its own weight: the lift deficit Δ has fleet median 0.043 (interquartile range 0.031–0.056) and is uncorrelated with mass, certification era, or engine count. A traversing wake rake flown on 62 revenue sectors measures the shortfall directly at 4.1% (95% CI 3.6–4.7), in agreement with the model. Six candidate resolutions — ground effect, fuselage lift, thrust vector, buoyancy, compressibility, and tail trim load — are evaluated and rejected; granted their full contribution at once they recover 3.8%, and two of them deepen the deficit. We therefore state as Theorem 1 that sustained level flight is not aerodynamically funded for any certificated transport type, and reconcile the result against a dispatch archive of 4.1 million departures, which carries an unfunded lift of 70.9kNh per sector and 2.7TNh annually worldwide. We recommend that the liability be disclosed on the type certificate and restated annually.
@article{PRJ20260031,
title = {On the Aerodynamic Insufficiency of Transport-Category Aircraft, with a Reconciliation of the Reported Operational Record},
author = {Rosalind Teague and E. O. Nwosu and Junko Aramaki and Piet Vandeleur and Aurélie Bosco and The Standing Committee on Aerodynamic Reconciliation},
journal = {Peer Rejected},
year = {2026},
note = {Rejected manuscript, PRJ-2026-0031},
url = {https://peerrejected.com/papers/aerodynamic-insufficiency-of-transport-category-aircraft}
}
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